Intershaft seal with centrifugal compensation
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F16J-015/02
F01D-011/00
F16J-015/32
F16J-015/44
F02C-007/28
F16J-015/16
출원번호
US-0898402
(2013-05-20)
등록번호
US-8820752
(2014-09-02)
발명자
/ 주소
Garrison, Glenn M.
Vasagar, Thurai Manik
출원인 / 주소
Stein Seal Company
대리인 / 주소
Crilly, Esquire, Michael
인용정보
피인용 횟수 :
4인용 특허 :
15
초록▼
A segmented intershaft seal assembly for use between inner and outer shafts within a turbine engine is presented. The intershaft seal assembly includes annular end rings, an annular seal element with an inverted “T”-shaped cross section, at least one resilient element, an annular spacer ring, carrie
A segmented intershaft seal assembly for use between inner and outer shafts within a turbine engine is presented. The intershaft seal assembly includes annular end rings, an annular seal element with an inverted “T”-shaped cross section, at least one resilient element, an annular spacer ring, carriers, counterweights, and hydrodynamic grooves. The intershaft seal assembly is secured to the inner shaft. The resilient element(s) biases seal segments away from the inner shaft toward the outer shaft. The counterweights are disposed about the seal segments and substantially negate forces imposed by the seal segments outward toward the outer shaft. The hydrodynamic grooves are disposed along an inner annular surface of the outer shaft and direct fluid onto an outer surface along the seal segments when the outer shaft rotates. The hydrodynamic grooves form a thin-film layer and non-contact seal that separates the seal segments from the outer shaft which otherwise provide a contact-type seal.
대표청구항▼
1. An intershaft seal assembly interposed between an inner shaft and an outer shaft about a common axis within a turbine engine so as to separate a low pressure side from a high pressure side comprising: (a) a pair of annular end rings disposed about and directly contacts said inner shaft;(b) an ann
1. An intershaft seal assembly interposed between an inner shaft and an outer shaft about a common axis within a turbine engine so as to separate a low pressure side from a high pressure side comprising: (a) a pair of annular end rings disposed about and directly contacts said inner shaft;(b) an annular seal element formed by at least two seal segments, each said seal segment has an inverted “T”-shaped cross section, said seal segments disposed between said annular end rings so that a portion of said inverted “T”-shaped cross section extends above said annular end rings in direction of said outer shaft, each said seal segment includes a pair of shoulders which extend from said seal segment between said annular end rings and said inner shaft;(c) at least one resilient element which biases said seal segments away from said inner shaft toward said outer shaft;(d) an annular spacer ring disposed about and directly contacts said inner shaft, said annular spacer ring disposed between and attached to said annular end rings, said annular seal element disposed about said annular spacer ring;(e) a pair of carriers disposed between said annular end rings about said annular seal element, said carriers directly contact said annular spacer ring;(f) at least two counterweights oppositely disposed about said seal segments, each said counterweight attached to one said carrier and contacts one said shoulder, said counterweights substantially negate forces acting on said seal segments outward toward said outer shaft; and(g) a plurality of hydrodynamic grooves disposed along an inner annular surface of said outer shaft, said hydrodynamic grooves direct fluid onto an outer surface along each said seal segment when said outer shaft rotates, said fluid forms a thin-film layer which separates said seal segments from said outer shaft. 2. The intershaft seal assembly of claim 1, wherein each said counterweight includes a mass arm and a contact arm oppositely disposed about a flange, said contact arm contacts one said shoulder, said mass arm rotatably responsive to rotation of said inner shaft, said counterweight rotates about said flange. 3. The intershaft seal assembly of claim 2, wherein said hydrodynamic grooves are arranged so that at least one said hydrodynamic groove communicates fluid onto said outer surface of each said seal segment. 4. The intershaft seal assembly of claim 2, wherein said inner annular surface along said outer shaft includes an insert comprised of a wear resistant material, said hydrodynamic grooves disposed along said wear resistant insert, said outer surface of said seal segments contacts said insert absent said thin-film layer. 5. The intershaft seal assembly of claim 2, wherein said hydrodynamic grooves are disposed along each said seal segment to form at least two groups, each said group includes at least two said hydrodynamic grooves. 6. The intershaft seal assembly of claim 2, wherein each said counterweight directly contacts a spring which biases said contact arm away from said outer shaft. 7. The intershaft seal assembly of claim 2, wherein each said shoulder includes at least one notch, one said contact arm disposed within each said notch. 8. The intershaft seal assembly of claim 2, wherein one said annular end ring includes at least one vent hole adjacent to said low pressure side. 9. The intershaft seal assembly of claim 2, wherein each seal segment includes a groove and a dam disposed along said outer surface, said dam adjacent to said low pressure side. 10. The intershaft seal assembly of claim 1, wherein each said counterweight includes at least two mass arms and at least two contact arms oppositely disposed about and attached to an arcuate member, said arcuate member directly contacts a socket along said carrier so as to be rotatable within said socket, said contact arms directly contact at least one said seal segment, said mass arms rotatably responsive to rotation of said inner shaft. 11. The intershaft seal assembly of claim 10, wherein said hydrodynamic grooves are arranged so that at least one said hydrodynamic groove communicates fluid onto said outer surface of each said seal segment. 12. The intershaft seal assembly of claim 10, wherein said inner annular surface along said outer shaft includes an insert comprised of a wear resistant material, said hydrodynamic grooves disposed along said wear resistant insert, said outer surface of said seal segments contacts said insert absent said thin-film layer. 13. The intershaft seal assembly of claim 10, wherein said hydrodynamic grooves are disposed along each said seal segment to form at least two groups, each said group includes at least two said hydrodynamic grooves. 14. The intershaft seal assembly of claim 10, wherein each said counterweight biases said contact arm away from said outer shaft. 15. The intershaft seal assembly of claim 10, wherein each said shoulder includes at least two notches, one said contact arm disposed within each said notch. 16. The intershaft seal assembly of claim 10, wherein one said annular end ring includes at least one vent hole adjacent to said low pressure side. 17. The intershaft seal assembly of claim 10, wherein each seal segment includes a groove and a dam disposed along said outer surface, said dam adjacent to said low pressure side.
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이 특허에 인용된 특허 (15)
Dourlens,Herve H.; Marshall,Dale F.; Auber,Philippe, Bearing assembly and method.
Stein Philip C. (c/o Stein Seal Company ; 20th St. & Indiana Ave. Philadelphia PA 19132), Centrifugally compensated seal for sealing between concentric shafts.
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