US5215434A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Apparatus for the adjustment of stator blades of a gas turbine
Assignee: MTU Aero Engines AG
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Filing: 1992-01-27
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Granted: 1993-06-01
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Expires: 2012-01-27
Abstract
Abstract Apparatus for the support and adjustment of stator blades of a gas turbine, in which an adjusting ring is connected to the stator blades by adjustment levers disposed outside the turbine housing. The adjusting ring is supported for rotation in the circumferential direction on a support ring, which has elastic resilience in the radial direction, the support ring being suspended on and centered in a movable manner on radial pins fixed in an outer housing of the turbine. The connection of the adjusting ring and the support ring is achieved by a ball-bearing which is pre-stressed. When the adjusting ring is displaced circumferentially, the stator blades are pivoted around suspension shafts by levers fixed to the shafts and connected to the adjusting ring for universal pivotal movement.
Inventors
- 👤 Christian Greune
- 👤 Helmut Gross
- 👤 Georg Zotz
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 17:13
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/162
Claims Analysis
Total Claims: 22
Claim 1
Independent Claim
184 words
Apparatus for the precise adjustment of stator blades of a gas turbine, said apparatus comprising: an inner turbine housing, an outer housing spaced radially outwards of said inner turbine housing, a plurality of circumferentially spaced pins secured to said outer housing and projecting radially inwards towards the inner turbine housing, a plurality of bushings, each slidably mounted on a respective said pin for travel along the axis of said pin, each said bushing having an outer curved surface, a support ring suspended on said bushings radially inwards of said outer housing, said support ring having openings with curved surfaces which are suspended on the curved surfaces of said bushings, an adjusting ring disposed between said support ring and said inner turbine housing, a plurality of circumferentially spaced rollers disposed between the support ring and the adjusting ring to rollably support the adjusting ring for circumferential movement, stator blade means pivotably supported in said inner housing, and lever means connecting said stator blade means to said adjusting ring to produce adjustable pivotal movement of said stator blade means upon circumferential movement of said adjusting ring.
Claim 2
Dependent Claim
184 words
Apparatus for the precise adjustment of stator blades of a gas turbine, said apparatus comprising: an inner turbine housing, an outer housing spaced radially outwards of said inner turbine housing, a plurality of circumferentially spaced pins secured to said outer housing and projecting radially inwards towards the inner turbine housing, a plurality of bushings, each slidably mounted on a respective said pin for travel along the axis of said pin, each said bushing having an outer curved surface, a support ring suspended on said bushings radially inwards of said outer housing, said support ring having openings with curved surfaces which are suspended on the curved surfaces of said bushings, an adjusting ring disposed between said support ring and said inner turbine housing, a plurality of circumferentially spaced rollers disposed between the support ring and the adjusting ring to rollably support the adjusting ring for circumferential movement, stator blade means pivotably supported in said inner housing, and lever means connecting said stator blade means to said adjusting ring to produce adjustable pivotal movement of said stator blade means upon circumferential movement of said adjusting ring.
Claim 3
Dependent Claim
19 words
Apparatus as claimed in claim 1, wherein said pins are circumferentially spaced at equal distances around said outer housing.
Claim 4
Dependent Claim
20 words
Apparatus as claimed in claim 2, wherein said support ring is shaped to be elastically deformable in the radial direction.
Claim 5
Dependent Claim
11 words
Apparatus as claimed in claim 2, wherein said rollers are spherical.
Claim 6
Dependent Claim
12 words
Apparatus as claimed in claim 4, comprising a cage supporting said rollers.
Claim 7
Dependent Claim
20 words
Apparatus as claimed in claim 5, wherein said cage is freely disposed between said adjusting ring and said support ring.
Claim 8
Dependent Claim
22 words
Apparatus as claimed in claim 4, wherein said spherical rollers are maintained between the adjusting ring and the support ring under stress.
Claim 9
Dependent Claim
21 words
Apparatus as claimed in claim 4, wherein said spherical rollers are made of a ceramic material which has low heat conductivity.
Claim 10
Dependent Claim
15 words
Apparatus as claimed in claim 8, wherein said ceramic material is hot pressed silicon nitride.
Claim 11
Dependent Claim
15 words
Apparatus as claimed in claim 2, wherein said curved surfaces of said bushings are spherical.
Claim 12
Dependent Claim
16 words
Apparatus as claimed in claim 2, wherein each said pin is disposed between two respective rollers.
Claim 13
Dependent Claim
14 words
Apparatus as claimed in claim 1, comprising thermal insulation means on said outer housing.
Claim 14
Dependent Claim
21 words
Apparatus as claimed in claim 1, comprising means for circumferentially displacing the adjusting ring to pivotably adjust the stator blade means.
Claim 15
Dependent Claim
45 words
Apparatus as claimed in claim 13, wherein said means for circumferentially displacing the adjusting ring comprises a rotatable input shaft and means coupling said input shaft with said adjusting ring for producing rotation of said adjusting ring in correspondence with rotation of said input shaft.
Claim 16
Dependent Claim
53 words
Apparatus as claimed in claim 1, wherein said stator blade means comprises a row of circumferentially spaced stator blades suspended in said inner housing, each stator blade including a shaft pivotal in said inner housing around an axis of the shaft, said lever means being coupled to the shafts of the stator blades.
Claim 17
Dependent Claim
52 words
Apparatus as claimed in claim 15, wherein said lever means comprises a pivotal rod for each stator blade, each pivotal rod having one end supported for universal pivotal movement in a fixed radial position in said adjusting ring and an opposite end fixedly connected to the shaft of the associated stator blade.
Claim 18
Dependent Claim
29 words
Apparatus as claimed in claim 16, wherein said stator blade means further comprises a second row of said stator blades connected by respective pivotal rods to said adjusting ring.
Claim 19
Dependent Claim
17 words
Apparatus as claimed in claim 1, wherein said support ring includes a portion having a rectangular cross-section.
Claim 20
Dependent Claim
133 words
Apparatus for the precise adjustment of pivotal stator blades of a gas turbine having an inner turbine housing surrounded by an outer housing, said apparatus comprising: a support ring disposed between the inner turbine housing and the outer housing, means supporting said support ring from the outer housing at a plurality of circumferentially spaced locations with capability at each said location of radial displacement and universal pivotal movement relative to said outer housing, an adjusting ring, roller bearing means supporting said adjusting ring on said support ring for relative circumferential rotation of said adjusting ring on said support ring, means for producing circumferential movement of said adjusting ring, and lever means connecting said adjusting ring to stator blades of said turbine to pivot said stator blades upon circumferential movement of said adjusting ring.
Claim 21
Dependent Claim
133 words
Apparatus for the precise adjustment of pivotal stator blades of a gas turbine having an inner turbine housing surrounded by an outer housing, said apparatus comprising: a support ring disposed between the inner turbine housing and the outer housing, means supporting said support ring from the outer housing at a plurality of circumferentially spaced locations with capability at each said location of radial displacement and universal pivotal movement relative to said outer housing, an adjusting ring, roller bearing means supporting said adjusting ring on said support ring for relative circumferential rotation of said adjusting ring on said support ring, means for producing circumferential movement of said adjusting ring, and lever means connecting said adjusting ring to stator blades of said turbine to pivot said stator blades upon circumferential movement of said adjusting ring.
Claim 22
Dependent Claim
47 words
Apparatus as claimed in claim 19 wherein said roller bearing means comprises a plurality of balls rollably supported between said support ring and said adjusting ring, said plurality of balls being arranged between said rings in circumferentially spaced relation and being engaged between said rings with pre-stress.
References Cited (Backward Citations)
US2718349A
Cited
US4003675A
Cited
US4130375A
Cited
US4035101A
Cited
US4139329A
Cited
US4363600A
Cited
JPS5859400A
Cited
US4618311A
Cited
US4755104A
Cited
US4810165A
Cited
US4836746A
Cited
US5035572A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1996-05-31 | 1996-11-30 | 1997-06-01 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2000-05-31 | 2000-11-30 | 2001-06-01 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2004-05-31 | 2004-11-30 | 2005-06-01 | $7700.00 | Window Closed / Lapsed |