Epicyclic geartrain
10690231 ยท 2020-06-23
Assignee
Inventors
Cpc classification
F02C7/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H1/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02K3/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B03C2201/18
PERFORMING OPERATIONS; TRANSPORTING
F16H57/0402
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H57/0486
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/98
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/40311
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H57/0404
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16H57/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02K3/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H1/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An epicyclic geartrain includes a debris collection arrangement. The epicyclic geartrain comprises a sun gear, a plurality of planet gears, with the plurality of planet gears being supported by a planet torque ring, and a ring gear. The planet gears meshingly surround the sun gear, and the ring gear meshingly surrounds the planet gears. At least one of the sun gear, the plurality of planet gears, and the ring gear, is provided with a plurality of permanent magnet portions, and a debris collection element. The plurality of magnet portions is arranged as a circumferential array across a side of the corresponding gear. The debris collection element extends along the side face of the gear. The debris collection element is slidably positioned against the side face, such that rotation of the gear causes the debris collection element to remove any ferromagnetic debris particles that are magnetically attached to the side face.
Claims
1. A debris collection arrangement for an epicyclic geartrain, the epicyclic geartrain comprising a sun gear; a plurality of planet gears, the plurality of planet gears supported by a planet torque ring; and a ring gear, the planet gears meshingly surround the sun gear, and the ring gear meshingly surrounds the planet gears, wherein at least one of the sun gear, and the plurality of planet gears, is provided with a plurality of permanent magnet portions, and a debris collection element, the plurality of magnet portions is arranged as a circumferential array, the debris collection element extends along a side face of the corresponding gear, and the debris collection element is slidably positioned against the side face, such that rotation of the gear causes the debris collection element to remove any ferromagnetic debris particles that are magnetically attached to the side face.
2. The debris collection arrangement as claimed in claim 1, wherein the debris collection element comprises a transfer portion and a collection portion, the transfer portion has, in sequence, a leading edge, a transfer surface, and a trailing edge, the leading edge being slidably positioned against the side face, the collection portion extends from the trailing edge, and the collection portion has a C-shaped cross-sectional profile in which an open portion of the C-shaped profile faces towards the transfer surface, such that rotation of the gear causes ferromagnetic debris particles that are magnetically attached to the side face to be transferred over the leading edge, onto the transfer surface, and across the trailing edge and into the collection portion.
3. The debris collection arrangement as claimed in claim 2, wherein one edge of the open portion of the C-shaped profile is contiguous with the trailing edge, and at least part of the inner volume of the C-shaped profile extends in a direction opposite to an outwardly facing side of the transfer surface.
4. The debris collection arrangement as claimed in claim 2, wherein the transfer surface is inclined relative to the side face of the corresponding gear.
5. The debris collection arrangement as claimed in claim 2, wherein the leading edge of the transfer portion extends radially along the side face of the corresponding gear.
6. The debris collection arrangement as claimed in claim 2, wherein a longitudinal axis of the collection portion extends radially along the side face of the corresponding gear.
7. The debris collection arrangement as claimed in claim 2, wherein the leading edge of the transfer portion extends along the side face of the corresponding gear at an offset angle to a radius of the gear.
8. The debris collection arrangement as claimed in claim 1, wherein each one of plurality of magnet portions is attached to the side face of the corresponding gear, and the debris collection element is positioned to slide over the plurality of magnet portions.
9. The debris collection arrangement as claimed in claim 1, wherein a radially outward end of the collection portion fluidly communicates with a filter element, and the filter element being in fluid communication with the oil reservoir for the epicyclic geartrain.
10. The debris collection arrangement as claimed in claim 1, wherein a radially outward end of the collection portion is provided with a magnetic debris collection plug.
11. A geared turbofan engine comprising: a fan; a core gas turbine engine; and an epicyclic gearbox, wherein the gearbox connects the fan to the core gas turbine engine, and the gearbox comprises an debris collection arrangement as claimed in claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) There now follows a description of an embodiment of the disclosure, by way of non-limiting example, with reference being made to the accompanying drawings in which:
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(9) It is noted that the drawings may not be to scale. The drawings are intended to depict only typical aspects of the disclosure, and therefore should not be considered as limiting the scope of the disclosure. In the drawings, like numbering represents like elements between the drawings.
DETAILED DESCRIPTION
(10) A typical arrangement of the epicyclic gearbox 30 used in a geared turbofan gas turbine engine 10 is shown in
(11) Referring to
(12) As illustrated in
(13) In the present embodiment, the epicyclic geartrain 30 is configured in a planetary configuration, in which the sun gear 110 rotates in a first direction 116, and the planet torque ring 122 (together with the plurality of planet gears 120) rotates in a second opposite direction 128, while the ring gear 130 remains stationary. The epicyclic geartrain 30 of the present disclosure may however equally be applied to epicyclic geartrain configurations of the star or differential form.
(14) The planet torque ring 122 is positioned in an axial plane. The planet torque ring 122 is axially offset from the ring gear 130 by an axial clearance 124.
(15) In the present embodiment the epicyclic geartrain 30 comprises five planet gears 120. As outlined above, other embodiments of the disclosure may comprise an alternative quantity, say four or six for example, of planet gears 120.
(16) Each of the planet gears 120 meshes with the sun gear 120, and the planet gears are positioned to surround the sun gear 110. The ring gear 130 meshes with each of the planet gears 120, and the ring gear 130 is positioned to surround the planet gears 120.
(17) The sun gear 110 and the ring gear 130 are positioned to be coaxial. The planet gears 120 are arranged in a circumferential array around the sun gear 110.
(18) Each of the sun gear 110, the planet gears 120, and the ring gear 130 is provided with a plurality of permanent magnet portions 140. For each of the sun gear 110, the planet gears 120, and the ring gear 130, the plurality of permanent magnet portions 140 are arranged as a circumferential array 142. In other words, each of the sun gear 110, the planet gears 120, and the ring gear 130, itself comprises a circumferential array of permanent magnet portions 140.
(19) In the present embodiment, each circumferential array 142 of permanent magnet portions 140 is integrally formed with a respective one of the sun gear 110, the planet gears 120, and the ring gear 130. In other words, the circumferential array 142 of permanent magnet portions 140 is embedded in the body of the respective sun gear 110, planet gear 120, and ring gear 130.
(20) In the present embodiment, the sun gear 110 and each of the planet gears 120 is provided with a debris collection element 150. In the case of the planet gears 120, each debris collection element 150 is located on the planet torque ring 122, with the debris collection element 150 directed radially outwardly. This orientation simplifies the flow 182 of debris particles and associated oil. However, the debris collection elements 150 may be oriented at positions other than radially outwardly.
(21) Each debris collection element 150 extends along a side face 112:121 of the corresponding sun gear 110 and planet gears 120. Each debris collection element 150 is slidably positioned against the side face 112:121.
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(23) In this embodiment, one edge 166 of the open portion 164 of the C-shaped cross-sectional profile 162 is contiguous with the trailing edge 159. The transfer surface 156 is inclined relative to the side face 112:121 by an inclination angle 158.
(24) The collection portion 160 of the debris collection element 150 has a longitudinal axis 170. In this embodiment, as illustrated in
(25) In an alternative arrangement, shown in
(26) Referring to
(27) The debris collection element 250 has a transfer portion 252 and a collection portion 260. As in the first embodiment, the transfer portion 252 has, in sequence, a leading edge 254, a transfer surface 256, and a trailing edge 259, with the leading edge 254 being slidably positioned against the side face 112:121. The collection portion 260 extends from the trailing edge 259, and has a C-shaped cross-sectional profile 262. An open portion 264 of the C-shaped cross-sectional profile 262 faces towards the transfer surface 256.
(28) One edge 266 of the open portion 264 of the C-shaped cross-sectional profile 262 is contiguous with the trailing edge 259. The transfer surface 256 is inclined relative to the side face 112:121 by an inclination angle 258. At least a part of the inner volume 268 of the C-shaped cross-sectional profile 262 extends in a direction opposite to an outwardly facing side 257 of the transfer surface 256.
(29) In use, ferromagnetic wear debris particles 180 that are generated by the epicyclic gearbox 30 become suspended in the volume of oil within the gearbox 30. The presence of the magnet portions 140 at the side faces 112:121 of the gears 110:120 result in these ferromagnetic debris particles 180 becoming attached by magnetic force to the side faces 112:121. The rotation of the gear 110:120 causes the debris collection element 150 to remove these ferromagnetic debris particles 180 by a scooping or scraping action.
(30) The inclination of the transfer surface 156:256 relative to the side face 112:121 results in the magnetic force on each debris particle 180 reducing as the particle 180 moves across the transfer surface 156:256 from the leading edge 154:254 to the trailing edge 159:259, because the particle 180 moves further away from the side face 112:121 in an axial direction.
(31) When the particles 180 reach the collection portion 160:260, they become trapped within the C-shaped cross-sectional profile 162:262. The C-shaped cross-sectional profile 162:262 reduces the magnetic field from the magnet portions 140, which assists the transit of the debris particles 180 into the collection portion 160:260.
(32) The debris particles may be retained within the debris collection element 150:250, which is then cleaned during routine maintenance of the gearbox 30. In an alternative arrangement, the flow of oil and debris particles 182 passes over a magnetic debris collection plug 194, as shown in the left hand view in
(33) Although some of the debris particles 180 may escape from the collection portion 160, the magnet portions 140 extending over the side face 112:121 of the gear 110:120 will quickly trap the particles 180, which will be recycled over the debris collection element 150.
(34) Various example embodiments of the invention are described herein. Reference is made to these examples in a non-limiting sense. They are provided to illustrate more broadly applicable aspects of the invention. Various changes may be made to the invention described and equivalents may be substituted without departing from the scope of the invention. Further, it will be appreciated by those with skill in the art that each of the individual variations described and illustrated herein has discrete components and features which may be readily separated from or combined with the features of any of the other several embodiments without departing from the scope of the present inventions. All such modifications are intended to be within the scope of claims associated with this disclosure.
(35) In addition, where a range of values is provided, it is understood that every intervening value, between the upper and lower limit of that range and any other stated or intervening value in that stated range, is encompassed within the invention.
(36) Except where mutually exclusive, any of the features may be employed separately or in combination with any other features and the disclosure extends to and includes all combinations and sub-combinations of one or more features described herein.
(37) The foregoing description of various aspects of the disclosure has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure to the precise form disclosed, and obviously, many modifications and variations are possible. Such modifications and variations that may be apparent to a person of skill in the art are included within the scope of the disclosure as defined by the accompanying claims.