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公开(公告)号:US09752536B2
公开(公告)日:2017-09-05
申请号:US14641682
申请日:2015-03-09
Applicant: Caterpillar Inc.
Inventor: Richard E. Annati , Gary W. Powers , Jeffrey W. McCormack , Thomas J. Williams
IPC: F02B33/44 , F16C27/00 , F01D25/18 , F04B35/00 , F02M25/07 , F01D25/16 , F16C33/76 , F16C35/067 , F02M26/04 , F16C19/18
CPC classification number: F02M26/04 , F01D25/16 , F05D2220/40 , F16C19/184 , F16C33/767 , F16C35/067 , F16C2360/24 , Y02T10/144
Abstract: A turbocharger includes a turbine, a compressor, and a bearing housing forming a bearing bore. A bearing arrangement is disposed between a shaft interconnecting the turbine and compressor wheels, and the bearing housing. The bearing arrangement includes an outer bearing race element and an inner bearing race element rotatably disposed within the outer bearing race element. The inner bearing race element forms a hollow extension extending up to the compressor wheel, the extension having a hollow cylindrical shape that surrounds a portion of the shaft that is connected on one end to the compressor wheel and at another end is disposed adjacent to a seat formed on the extension portion around the shaft, and a nut engaged on the shaft and disposed within the extension at an offset distance from the seat.
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公开(公告)号:US20160265385A1
公开(公告)日:2016-09-15
申请号:US14641931
申请日:2015-03-09
Applicant: Caterpillar Inc.
Inventor: Richard E. Annati , Thomas J. Williams , Mark Suchezky
IPC: F01D25/16 , F16C33/58 , F16C33/76 , F02B33/40 , F04D29/42 , F02B39/04 , F01D5/02 , F01D25/24 , F04D29/28 , F16C35/06 , F02B37/00
CPC classification number: F01D25/16 , F01D5/02 , F01D25/24 , F02B33/40 , F02B37/00 , F02B39/04 , F04D29/059 , F04D29/266 , F04D29/284 , F05D2220/40 , F05D2240/24 , F05D2240/54 , F05D2240/60 , F16C19/548 , F16C35/063 , F16C35/067 , F16C2360/24 , F16J15/16 , Y02T10/144
Abstract: A turbocharger is provided that includes a turbine, a compressor and a bearing housing disposed and connected between the turbine and the compressor. A shaft is rotatably disposed within the bearing housing and extending into the turbine and the compressor. A bearing arrangement is disposed between the shaft and the bearing housing and includes a inner bearing race element and an outer bearing race element. The compressor wheel includes a hub having a collar portion with a bore therein for receiving an end of the shaft. An end portion of the inner bearing race element is arranged to engage an outer circumferential surface of the collar portion.
Abstract translation: 提供一种涡轮增压器,其包括涡轮机,压缩机和布置并连接在涡轮机和压缩机之间的轴承箱。 轴可旋转地设置在轴承壳体内并延伸到涡轮机和压缩机中。 轴承布置在轴和轴承壳体之间,并且包括内轴承座圈和外轴承座圈元件。 压缩机叶轮包括具有轴环部分的轮毂,该轴环部分具有用于容纳轴的端部的孔。 内轴承座圈元件的端部布置成接合套环部分的外圆周表面。
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公开(公告)号:US20160281645A1
公开(公告)日:2016-09-29
申请号:US14641665
申请日:2015-03-09
Applicant: Caterpillar Inc.
Inventor: Richard E. Annati , Gary W. Powers , Jeffrey W. McCormack , Gregg Williams , Thomas J. Williams
IPC: F02B33/44 , F01D25/16 , F04D29/056
CPC classification number: F02M26/04 , F01D25/16 , F01D25/183 , F01D25/24 , F02B37/00 , F02B39/14 , F02M26/05 , F04D25/024 , F04D29/059 , F05D2220/40 , F16C19/184 , F16C27/045 , F16C33/767 , F16C35/063 , F16C2360/24 , Y02T10/144
Abstract: A turbocharger includes a turbine, a compressor, and a bearing housing forming a bearing bore. A bearing arrangement is disposed between a shaft interconnecting the turbine and compressor wheels, and the bearing housing. The bearing arrangement includes first and second bearings formed between an outer bearing race element disposed within the bearing bore an inner bearing race element disposed within the outer bearing race element and between the outer bearing race element and the shaft. The inner bearing race element rotates with the shaft and forms an extension segment having an open channel that, together with an annular surface on an inner side of a back of the compressor wheel, forms a U-shaped channel into which a ring seal is disposed. The ring seal sealably engages the inner bearing race element and also slidably and sealably engages the inner bore of the bearing retainer.
Abstract translation: 涡轮增压器包括涡轮机,压缩机和形成轴承孔的轴承壳体。 轴承装置设置在连接涡轮和压缩机叶轮之间的轴与轴承壳体之间。 轴承装置包括形成在设置在轴承孔内的外轴承座圈元件之间的第一和第二轴承,设置在外轴承座圈内的内轴承座圈元件和外轴承座圈元件与轴之间。 内部轴承座圈与轴一起旋转并形成具有开放通道的延伸段,该通道与压缩机叶轮后部的内侧上的环形表面一起形成U形通道,环形密封件设置在该U形通道中 。 环形密封件可密封地接合内部轴承座圈元件,并且还可滑动地且可密封地接合轴承保持器的内孔。
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公开(公告)号:US09915172B2
公开(公告)日:2018-03-13
申请号:US14641931
申请日:2015-03-09
Applicant: Caterpillar Inc.
Inventor: Richard E. Annati , Thomas J. Williams , Mark Suchezky
IPC: F02B33/44 , F01D25/16 , F02B33/40 , F02B37/00 , F02B39/04 , F01D5/02 , F01D25/24 , F04D29/28 , F04D29/059 , F04D29/26 , F16C35/063 , F16C35/067 , F16J15/16 , F16C19/54
CPC classification number: F01D25/16 , F01D5/02 , F01D25/24 , F02B33/40 , F02B37/00 , F02B39/04 , F04D29/059 , F04D29/266 , F04D29/284 , F05D2220/40 , F05D2240/24 , F05D2240/54 , F05D2240/60 , F16C19/548 , F16C35/063 , F16C35/067 , F16C2360/24 , F16J15/16 , Y02T10/144
Abstract: A turbocharger is provided that includes a turbine, a compressor and a bearing housing disposed and connected between the turbine and the compressor. A shaft is rotatably disposed within the bearing housing and extending into the turbine and the compressor. A bearing arrangement is disposed between the shaft and the bearing housing and includes a inner bearing race element and an outer bearing race element. The compressor wheel includes a hub having a collar portion with a bore therein for receiving an end of the shaft. An end portion of the inner bearing race element is arranged to engage an outer circumferential surface of the collar portion.
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公开(公告)号:US20160281644A1
公开(公告)日:2016-09-29
申请号:US14641660
申请日:2015-03-09
Applicant: Caterpillar Inc.
Inventor: Richard E. Annati , Thomas J. Williams
IPC: F02B33/44 , F04D29/056 , F01D25/16
CPC classification number: F02M26/04 , F01D25/16 , F02B37/00 , F04D29/059 , F04D29/4206 , F05D2220/40 , F16C19/184 , F16C33/586 , F16C33/588 , F16C33/60 , F16C33/6651 , F16C33/6659 , F16C33/767 , F16C33/80 , F16C2240/70 , F16C2360/24
Abstract: A turbocharger includes a turbine, a compressor, and a bearing housing forming a bearing bore. A bearing arrangement is disposed between a shaft interconnecting the turbine and compressor wheels, and the bearing housing. The bearing arrangement includes first and second bearings formed between an outer bearing race element disposed within the bearing bore an inner bearing race element disposed within the outer bearing race element and between the outer bearing race element and the shaft. The inner bearing race element includes a flared portion extending radially outwardly to provide torsional and bending rigidity to the shaft.
Abstract translation: 涡轮增压器包括涡轮机,压缩机和形成轴承孔的轴承壳体。 轴承装置设置在连接涡轮和压缩机叶轮之间的轴与轴承壳体之间。 轴承装置包括形成在设置在轴承孔内的外轴承座圈元件之间的第一和第二轴承,设置在外轴承座圈内的内轴承座圈元件和外轴承座圈元件与轴之间。 内轴承座元件包括径向向外延伸的扩张部分,以向轴提供扭转和弯曲刚性。
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公开(公告)号:US09777747B2
公开(公告)日:2017-10-03
申请号:US14642621
申请日:2015-03-09
Applicant: Caterpillar Inc.
Inventor: Richard E. Annati , Gary W. Powers , Jeffrey W. McCormack , Thomas J. Williams
IPC: F04D29/62 , F04D29/42 , F04D29/059 , F02C6/12 , F01D25/28
CPC classification number: F04D29/624 , F01D25/28 , F01D25/285 , F02C6/12 , F04D29/059 , F04D29/4206 , F05D2220/40 , F05D2230/68 , F05D2250/281 , F05D2260/31
Abstract: A housing for a turbocharger includes a first outer surface, a second outer surface opposite the first outer surface, and a mounting hole extending between the first outer surface and the second outer surface. The mounting hole includes a first end opposite a second end and a counterbore formed at the first end. The counterbore includes threads that are configured to engage with threads on a shank of a lifting device. The mounting hole also includes a throughbore extending from the counterbore to the second end and configured to receive a fastener for mounting the turbocharger housing. The counterbore forms a first opening through the first outer surface of the turbocharger housing, and the throughbore forms a second opening through the second outer surface of the turbocharger housing. The mounting hole is configured to receive only one fastener or shank at a time.
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公开(公告)号:US09739238B2
公开(公告)日:2017-08-22
申请号:US14641660
申请日:2015-03-09
Applicant: Caterpillar Inc.
Inventor: Richard E. Annati , Thomas J. Williams
IPC: F02B33/44 , F16C27/00 , F01D25/18 , F04B35/00 , F02M25/07 , F01D25/16 , F04D29/059 , F04D29/42 , F16C19/18 , F16C33/58 , F16C33/66 , F16C33/76 , F16C33/80
CPC classification number: F02M26/04 , F01D25/16 , F02B37/00 , F04D29/059 , F04D29/4206 , F05D2220/40 , F16C19/184 , F16C33/586 , F16C33/588 , F16C33/60 , F16C33/6651 , F16C33/6659 , F16C33/767 , F16C33/80 , F16C2240/70 , F16C2360/24
Abstract: A turbocharger includes a turbine, a compressor, and a bearing housing forming a bearing bore. A bearing arrangement is disposed between a shaft interconnecting the turbine and compressor wheels, and the bearing housing. The bearing arrangement includes first and second bearings formed between an outer bearing race element disposed within the bearing bore an inner bearing race element disposed within the outer bearing race element and between the outer bearing race element and the shaft. The inner bearing race element includes a flared portion extending radially outwardly to provide torsional and bending rigidity to the shaft.
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公开(公告)号:US09683520B2
公开(公告)日:2017-06-20
申请号:US14641665
申请日:2015-03-09
Applicant: Caterpillar Inc.
Inventor: Richard E. Annati , Gary W. Powers , Jeffrey W. McCormack , Gregg Williams , Thomas J. Williams
IPC: F02B33/44 , F04B17/00 , F04B35/00 , F16C27/00 , F16C19/00 , F16C43/04 , F01D25/18 , F02M25/07 , F02B37/00 , F02B39/14 , F04D25/02 , F04D29/059 , F01D25/16 , F01D25/24 , F02M26/05
CPC classification number: F02M26/04 , F01D25/16 , F01D25/183 , F01D25/24 , F02B37/00 , F02B39/14 , F02M26/05 , F04D25/024 , F04D29/059 , F05D2220/40 , F16C19/184 , F16C27/045 , F16C33/767 , F16C35/063 , F16C2360/24 , Y02T10/144
Abstract: A turbocharger includes a turbine, a compressor, and a bearing housing forming a bearing bore. A bearing arrangement is disposed between a shaft interconnecting the turbine and compressor wheels, and the bearing housing. The bearing arrangement includes first and second bearings formed between an outer bearing race element disposed within the bearing bore an inner bearing race element disposed within the outer bearing race element and between the outer bearing race element and the shaft. The inner bearing race element rotates with the shaft and forms an extension segment having an open channel that, together with an annular surface on an inner side of a back of the compressor wheel, forms a U-shaped channel into which a ring seal is disposed. The ring seal sealably engages the inner bearing race element and also slidably and sealably engages the inner bore of the bearing retainer.
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公开(公告)号:US20160281648A1
公开(公告)日:2016-09-29
申请号:US14641682
申请日:2015-03-09
Applicant: CATERPILLAR INC.
Inventor: Richard E. Annati , Gary W. Powers , Jeffrey W. McCormack , Thomas J. Williams
CPC classification number: F02M26/04 , F01D25/16 , F05D2220/40 , F16C19/184 , F16C33/767 , F16C35/067 , F16C2360/24 , Y02T10/144
Abstract: A turbocharger includes a turbine, a compressor, and a bearing housing forming a bearing bore. A bearing arrangement is disposed between a shaft interconnecting the turbine and compressor wheels, and the bearing housing. The bearing arrangement includes an outer bearing race element and an inner bearing race element rotatably disposed within the outer bearing race element. The inner bearing race element forms a hollow extension extending up to the compressor wheel, the extension having a hollow cylindrical shape that surrounds a portion of the shaft that is connected on one end to the compressor wheel and at another end is disposed adjacent to a seat formed on the extension portion around the shaft, and a nut engaged on the shaft and disposed within the extension at an offset distance from the seat.
Abstract translation: 涡轮增压器包括涡轮机,压缩机和形成轴承孔的轴承壳体。 轴承装置设置在连接涡轮和压缩机叶轮之间的轴与轴承壳体之间。 轴承装置包括外轴承座圈和可旋转地设置在外轴承座圈元件内的内轴承座圈元件。 内部轴承座圈形成延伸到压缩机叶轮的中空延伸部,该延伸部具有中空圆柱形形状,该中空圆柱形围绕轴的一部分连接到压缩机叶轮上,另一端邻近座椅 形成在所述轴周围的延伸部分上,以及螺母,其接合在所述轴上并且在所述延伸部内以距离所述座部偏移的距离设置。
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