Retention of ball bearing cartridge for turbomachinery
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F16C-019/08
F16C-023/06
F16C-033/66
출원번호
US-0180696
(2011-07-12)
등록번호
US-8454242
(2013-06-04)
발명자
/ 주소
Mavrosakis, Peter
출원인 / 주소
Honeywell International Inc.
대리인 / 주소
Pangrle, Brian J.
인용정보
피인용 횟수 :
17인용 특허 :
20
초록▼
An assembly for a turbocharger includes a ball bearing cartridge, a center housing with a bore, a turbine end counterbore and a compressor end surface that includes a recess, and a compressor backplate with an axial extension configured to fit into the recess where the counterbore and the backplate
An assembly for a turbocharger includes a ball bearing cartridge, a center housing with a bore, a turbine end counterbore and a compressor end surface that includes a recess, and a compressor backplate with an axial extension configured to fit into the recess where the counterbore and the backplate define, at least in part, an axial length of a bearing cartridge chamber. Various other devices, assemblies, etc., are also disclosed.
대표청구항▼
1. An assembly for a turbocharger, the assembly comprising: a ball bearing cartridge that comprises two sets of rolling elements and an outer race wherein the outer race comprises a center section surface having a center section diameter, two intermediate section surfaces having an intermediate sect
1. An assembly for a turbocharger, the assembly comprising: a ball bearing cartridge that comprises two sets of rolling elements and an outer race wherein the outer race comprises a center section surface having a center section diameter, two intermediate section surfaces having an intermediate section diameter and two outer section surfaces having an outer section diameter, the sections disposed along an axial length defined by two opposing ends of the outer race,step transitions, each of the step transitions positioned between a respective one of the outer section surfaces and a respective one of the intermediate section surfaces, andtwo wells, each of the wells positioned between the center section surface and a respective one of the intermediate section surfaces, wherein each of the wells comprises a lubricant channel to direct lubricant to a respective set of the two sets of rolling elements;a center housing that comprises a lubricant inlet,an inner wall that defines a bore wherein the inner wall comprises a lubricant opening to receive lubricant from the lubricant inlet, a first inner surface having a first inner diameter, and a second inner surface having a second inner diameter wherein the first inner diameter exceeds the second inner diameter,a turbine end counterbore having a counterbore inner diameter wherein the section diameters of the outer race exceed the counterbore inner diameter, anda compressor end surface that comprises a recess; anda compressor backplate that comprises an axial extension configured to fit into the recess wherein the axial extension comprises an opening having an inner diameter less than the section diameters of the outer race;wherein the counterbore and the backplate define an axial length of a bearing cartridge chamber wherein the axial length of the chamber exceeds the axial length of the outer race to provide clearance between the outer race and the chamber. 2. The assembly of claim 1 further comprising a feature to adjust clearance between the outer race and the chamber, the feature being disposed between the backplate and the housing. 3. The assembly of claim 2 wherein the feature comprises a gasket. 4. The assembly of claim 2 wherein the feature comprises a spacer. 5. The assembly of claim 1 wherein the outer race of the ball bearing cartridge comprises an opening for drainage of lubricant. 6. The assembly of claim 1 wherein the outer race of the ball bearing cartridge comprises an opening for receipt of a locating pin. 7. An assembly comprising: a turbocharger center housing that comprises a lubricant inlet,an inner wall that defines a bore having an axis extending from a compressor side to a turbine side of the housing wherein the inner wall comprises, positioned in an axial direction toward the compressor side, a lubricant opening to receive lubricant from the lubricant inlet, a first inner surface having a first inner diameter, and a second inner surface having a second inner diameter wherein the first inner diameter exceeds the second inner diameter,a turbine end counterbore having a counterbore inner diameter wherein the first inner diameter and the second inner diameter of the bore defined by the inner wall exceed the counterbore inner diameter, anda compressor end surface that comprises a recess; anda compressor backplate that comprises an axial extension configured to fit into the recess wherein the axial extension comprises an opening having an inner dimension wherein the first inner diameter and the second inner diameter of the bore defined by the inner wall exceed the inner dimension of the axial extension;wherein the counterbore and the backplate define, at least in part, an axial length of a bearing cartridge chamber. 8. The assembly of claim 7 further comprising a feature to adjust the axial length of the bearing cartridge chamber, the feature being disposed between the backplate and the housing. 9. The assembly of claim 8 wherein the feature comprises a gasket. 10. The assembly of claim 8 wherein the feature comprises a spacer.
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이 특허에 인용된 특허 (20)
Kronenberger Alban (Schweinfurt DEX) Bayer Oswald (Aidhausen DEX), Anti-friction bearing for heat resistance.
Aguilar Scott Grover ; Elpern David George ; Hebben Peter John ; Jensen Lloyd Bill ; Coleman Steven Walter ; Sahay Sunhil Nandan ; Milliken Douglas Alan ; Lopez Raymond Leo ; Wick Werner, Turbocharger integrated bearing system.
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