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US4295784A Expired / Lapsed US ⏱️ 0.0 years remaining

Variable stator

Assignee: RTX Corp
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Filing: 1979-09-26
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Granted: 1981-10-20
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Expires: 1999-09-26
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Abstract

Abstract The linkage system for a variable stator vane is made to achieve different rates between stages of stators in a variable stator configuration for an axial flow compressor of a turbine type power plant. The actuator-linkage arrangement permits nesting of the actuator providing a compact design.

Inventors

  • 👤 Frank B. Manning

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 15:20
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/162; F01D17/20

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 194 words
A stator vane actuation system for a compressor of a gas turbine engine including a plurality of axially spaced rows of circumferentially pivotally mounted vanes, an actuator having a connecting rod, a synchronizing ring for each row of vanes mounted external of the engine connecting each vane for pivotal movement, means interconnecting said connecting rod and at least one of said synchronizing rings for positioning each of said vanes in said row upon actuation of said actuator, linkage means connecting said interconnecting means and at least a second synchronizing ring so that actuating said actuator positions said one synchronizing ring for moving said one row of vanes at a given rate and the movement of said second synchronizing ring for moving the attached row of vanes to said second synchronizing ring at a different rate, a fixed elongated member, bell crank means for each of said synchronizing rings pivotally mounted on said fixed elongated member, means interconnecting said bell crank and said synchronizing rings, the bell crank means actuating said one synchronizing ring and the bell crank means actuating said second synchronizing ring being disposed at respectively different angles relative to said elongated member.
Claim 2
Dependent Claim 194 words
A stator vane actuation system for a compressor of a gas turbine engine including a plurality of axially spaced rows of circumferentially pivotally mounted vanes, an actuator having a connecting rod, a synchronizing ring for each row of vanes mounted external of the engine connecting each vane for pivotal movement, means interconnecting said connecting rod and at least one of said synchronizing rings for positioning each of said vanes in said row upon actuation of said actuator, linkage means connecting said interconnecting means and at least a second synchronizing ring so that actuating said actuator positions said one synchronizing ring for moving said one row of vanes at a given rate and the movement of said second synchronizing ring for moving the attached row of vanes to said second synchronizing ring at a different rate, a fixed elongated member, bell crank means for each of said synchronizing rings pivotally mounted on said fixed elongated member, means interconnecting said bell crank and said synchronizing rings, the bell crank means actuating said one synchronizing ring and the bell crank means actuating said second synchronizing ring being disposed at respectively different angles relative to said elongated member.
Claim 3
Dependent Claim 60 words
A stator vane actuating system as in claim 1 including a connecting lever interconnecting each of said vanes in a given row to its respective synchronizing ring, the direction of connecting the vanes of the first of said axially spaced rows being in allochiral relationship with the direction of connecting the vanes of the last of said axially spaced rows.
Claim 4
Dependent Claim 28 words
A stator vane actuation system as in claim 2 wherein said actuator is disposed between said first of said axially spaced rows and said last axially spaced rows.
Claim 5
Dependent Claim 33 words
A stator vane actuation system as in claim 2 including a connecting link interconnecting each of said bell cranks and said synchronizing rings and said actuator being supported to said fixed elongated member.

References Cited (Backward Citations)

US2858052A Cited
US3066488A Cited
US3458118A Cited
GB2003988A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-10-19 1985-04-20 1985-10-20 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-10-19 1989-04-20 1989-10-20 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-10-19 1993-04-20 1993-10-20 $7700.00 Window Closed / Lapsed

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