Guide vane arrangement and method for mounting a guide vane
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-009/02
F01D-017/16
F01D-011/00
출원번호
US-0305134
(2014-06-16)
등록번호
US-9617861
(2017-04-11)
우선권정보
DE-10 2013 211 629 (2013-06-20)
발명자
/ 주소
Klaen, Stephan
Schinko, Norbert
출원인 / 주소
MTU AERO ENGINES AG
대리인 / 주소
Barlow, Josephs & Holmes, Ltd.
인용정보
피인용 횟수 :
0인용 특허 :
3
초록▼
The invention relates to a guide vane arrangement and a method for mounting a guide vane. The guide vane arrangement has at least one guide vane having a radially inner journal, which engages in a borehole of a bushing. The bushing is disposed in a borehole of an inner ring segment. The journal is c
The invention relates to a guide vane arrangement and a method for mounting a guide vane. The guide vane arrangement has at least one guide vane having a radially inner journal, which engages in a borehole of a bushing. The bushing is disposed in a borehole of an inner ring segment. The journal is connected to the bushing in a rotation-resistant manner and a slide mounting is provided between the bushing and the inner ring borehole. For mounting the guide vane in an inner ring segment, the journal of the guide vane is introduced into the borehole of the bushing. Further, the journal is fastened to the bushing in a rotation-resistant manner, and the bushing is slide-mounted with the inner ring segment. The slide mounting is conducted prior to or simultaneously with or after the fastening of the journal to the bushing in a rotation-resistant manner.
대표청구항▼
1. A guide vane arrangement having at least one guide vane (110) with a radial inner journal (111), which engages in a borehole of a bushing (3), which is disposed in a second borehole of an inner ring segment (2), wherein a rotation-resistant connection is present between the journal (111) and the
1. A guide vane arrangement having at least one guide vane (110) with a radial inner journal (111), which engages in a borehole of a bushing (3), which is disposed in a second borehole of an inner ring segment (2), wherein a rotation-resistant connection is present between the journal (111) and the bushing (3) and a slide mounting is present between the bushing (3) and the borehole of the inner ring segment (2), wherein the journal (111) has an outer thread and the bushing (3) has an inner thread screwed therewith providing a screw connection; and a screw locking device to secure the screw connection of the journal (111) to the bushing (3); a threaded sleeve disposed between the journal (111) and the bushing (3), and the journal (111) and the bushing (3) being connected to the threaded sleeve; the bushing (3), with journal (111) secured thereto, with threaded sleeve disposed therebetween, being freely rotatable within the second borehole of the inner ring segment (2) thereby permitting adjustment of the guide vane (110), attached to the radial inner journal (111), about its longitudinal axis. 2. The guide vane arrangement according to claim 1, wherein the outer thread of the journal (111) is screwed with a nut inner thread of a nut. 3. The guide vane arrangement according to claim 1, wherein the screw locking device has a split pin locking device (33) and/or a locking pin (7) and/or a snap ring locking device and/or a locking wire (8). 4. The guide vane arrangement according to claim 1, wherein the inner ring segment (2) is detachably connected to a seal support segment (4). 5. The guide vane arrangement according to claim 1, wherein at least one additional, outer guide vane (110), in the circumferential direction of the inner ring segment, which is distanced in the peripheral direction, having an additional radially inner journal (111), which engages in a first additional borehole of an additional bushing (3), which is disposed in a second additional borehole of the inner ring segment (2), wherein the additional journal (111) and the additional bushing (3) are connected in a rotation-resistant manner, and the additional bushing (3) is slide-mounted in the second additional borehole of the inner ring segment (2). 6. The guide vane arrangement according to claim 1, wherein at least one additional, inner guide vane (110), in the circumferential direction of the inner ring segment, which is adjacent in the peripheral direction, having an additional radially inner journal (111), which engages in an additional borehole of an additional bushing (3), which is disposed in a second additional borehole of the inner ring segment (2), wherein the additional journal (111) is slide-mounted in the additional bushing (3) and/or the additional bushing (3) is slide-mounted in the second additional borehole of the inner ring segment (2). 7. A guide vane arrangement of claim 1, wherein the guide vane is configured for use in a gas turbine having at least one compressor stage and/or turbine stage. 8. A method for fastening a guide vane (110) to an inner ring segment (2), comprising the steps of: providing a guide vane with a journal (111);providing a bushing with a first borehole;providing an inner ring segment with a second borehole;providing a threaded sleeve between the journal (111) and the bushing (3) with the journal (111) and the bushing (3) being connected to the threaded sleeve;introducing the journal (111) of the guide vane (110) into the first borehole of the bushing (3) with the threaded sleeve residing therebetween,prior to, simultaneously with, or subsequently arranging the bushing in the second borehole of the inner ring segment (2);prior to, simultaneously with, or subsequently attaching the journal (111) to the bushing (3) in a rotation-resistant manner; andslide-mounting the bushing (3), with journal (111) secured thereto, within the second borehole of the inner ring segment (2) to adjust the guide vane (110), attached to the radial inner journal (111), about its longitudinal axis.
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이 특허에 인용된 특허 (3)
Agram Daniel Andre,FRX ; Marlin Anne-Cecile Christine,FRX, Circular stage of vanes connected at internal ends thereof by a connecting ring.
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