Thrust bearing shaft for thrust and journal air bearing cooling in an air machine
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F15D-001/00
출원번호
US-0974063
(2010-12-21)
등록번호
US-8517665
(2013-08-27)
발명자
/ 주소
Lugo, Valentina
Colson, Darryl A.
Beers, Craig M.
출원인 / 주소
Hamilton Sundstrand Corporation
대리인 / 주소
Carlson, Gaskey & Olds, PC
인용정보
피인용 횟수 :
23인용 특허 :
11
초록▼
A thrust bearing shaft has a radially enlarged thrust disk to be mounted between two static housing surfaces in an air cycle machine. A first portion of the thrust bearing shaft extends from a first face of the thrust disk. A second portion extends from a second opposed face of the thrust disk. The
A thrust bearing shaft has a radially enlarged thrust disk to be mounted between two static housing surfaces in an air cycle machine. A first portion of the thrust bearing shaft extends from a first face of the thrust disk. A second portion extends from a second opposed face of the thrust disk. The second portion has sealing ribs and six holes. The sealing ribs are spaced closer to the thrust disk than are the holes. A ratio of a distance from an end of the second portion to a center of the holes compared to a distance from the end of the second portion to the second face of the thrust disk is between 0.20 and 0.22. In addition, an air cycle machine incorporating the thrust bearing shaft, and a method of assembling the thrust bearing shaft into an air cycle machine are disclosed.
대표청구항▼
1. A thrust bearing shaft comprising: a body having a radially enlarged thrust disk to be mounted between two static housing surfaces in an air cycle machine, and provides thrust bearing surfaces;a first portion of the thrust bearing shaft extending from one face of said thrust disk;a second portion
1. A thrust bearing shaft comprising: a body having a radially enlarged thrust disk to be mounted between two static housing surfaces in an air cycle machine, and provides thrust bearing surfaces;a first portion of the thrust bearing shaft extending from one face of said thrust disk;a second portion of the thrust bearing shaft extending from an opposed second face of said thrust disk, and said second portion having sealing ribs, and six holes extending through a body of said thrust bearing shaft to a hollow interior, said sealing ribs being spaced closer to said thrust disk than are said holes; anda ratio of a distance from an end of said second portion remote from said thrust disk to a center of said holes to a distance from the end of said second portion to the second face of said thrust disk being between 0.20 and 0.22. 2. The thrust bearing shaft as set forth in claim 1, wherein a ratio of a diameter of said holes to a radius to the second portion of said thrust bearing shaft at a location of said holes being between 0.508 and 0.537. 3. The thrust bearing shaft as set forth in claim 2, wherein a ratio of a diameter of said holes to a radius to an outer periphery of said thrust disk being between 0.140 and 0.147. 4. The thrust bearing shaft as set forth in claim 2, wherein said second portion includes two sub-portions with a first sub-portion including said holes and said sealing ribs, and a second sub-portion spaced between said first sub-portion and said disk, and said second sub-portion having a greater outer diameter than said first sub-portion. 5. An air cycle machine comprising: a compressor rotor and a turbine rotor secured to rotate together; andan air bearing system including an inlet for supplying air into a housing, air flowing through a chamber in the housing along two thrust bearing surfaces, said thrust bearing surfaces being defined between a housing, and a disk on a thrust bearing shaft, said thrust bearing shaft including the disk, a first portion of the thrust bearing shaft extending from one face of said disk, a second portion of the thrust bearing shaft extending from an opposed second face of said disk, and said second portion having sealing ribs, and six holes extending through a body of said thrust bearing shaft to a hollow interior, said sealing ribs being spaced closer to said disk than said holes; anda ratio of a distance from an end of said second portion remote from said disk to a center of said holes to a distance from the end of said second portion to the second face of said disk being between 0.20 and 0.22. 6. The air cycle machine as set forth in claim 5, wherein a ratio of a diameter of said holes to a radius to the second portion of said thrust bearing shaft at a location of said holes being between 0.508 and 0.537. 7. The air cycle machine as set forth in claim 6, wherein a ratio of a diameter of said holes to a radius to an outer periphery of said disk being between 0.140 and 0.147. 8. The air cycle machine as set forth in claim 6, wherein said second portion includes two sub-portions with a first sub-portion including said holes and said sealing ribs, and a second sub-portion spaced between said first sub-portion and said disk, and said second sub-portion having a greater outer diameter than said first sub-portion. 9. The air cycle machine as set forth in claim 5, wherein journal bearings supporting the thrust bearing shaft in the housing, and supporting a second shaft within the housing, with air passing along each of said thrust bearing surfaces, and then along said journal bearings. 10. The air cycle machine as set forth in claim 9, wherein the first portion of said thrust bearing shaft being secured to an end of said second shaft. 11. A method of assembling a thrust bearing shaft into an air cycle machine comprising the steps of: providing a thrust bearing shaft having a radially enlarged thrust disk to be mounted between two static housing surfaces in an air cycle machine, a first portion of the thrust bearing shaft extending from one face of said thrust disk, a second portion of the thrust bearing shaft extending from an opposed second face of said thrust disk, and said second portion having sealing ribs, and six holes extending through a body of said thrust bearing shaft to a hollow interior, said sealing ribs being spaced closer to said thrust disk than are said holes, a ratio of a distance from an end of said second portion remote from said thrust disk to a center of said holes to a distance from the end of said second portion to the second face of said thrust disk being between 0.20 and 0.22;inserting said thrust bearing shaft into a housing with said thrust disk being positioned between housing portions to define the thrust bearing surfaces; andsecuring the first portion of said thrust bearing shaft to an end of a second shaft.
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이 특허에 인용된 특허 (11)
McAuliffe,Christopher; Beers,Craig M.; Zywiak,Thomas, Air bearing and motor cooling.
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