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US3685921A Expired / Lapsed US ⏱️ 0.0 years remaining

Gas turbine with variable blade distributor

Assignee: Bennes Marrel SA
•
Filing: 1970-08-05
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Granted: 1972-08-22
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Expires: 1990-08-05
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Abstract

Abstract An annular guide ring between a high pressure turbine rotor and a low pressure turbine rotor is provided with pivotal blades operable by a common ring gear and biased radially inwardly against an inner annular casing by a spring surrounding the pivot shaft of each blade.

Inventors

  • 👤 Lucien Dekeyser

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 12:04
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/162; F05; F05D; F05D2250/00; F05D2250/20; F05D2250/24; F05D2250/241; F05D2260/00; F05D2260/50; F05D2260/53; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 160 words
In a gas turbine of the type having a high pressure turbine rotor, a low pressure turbine rotor and an intermediate annular guide ring disposed coaxially in a casing wherein said guide ring includes a plurality of blades each of which is mounted for rotation about an individual radially extending axis by means of a common gear ring disposed in meshing engagement with a pinion coaxially secured to each blade with each blade bearing on an inner spherical surface of said casing, the improvement comprising a plurality of stepped shaft means each having a pinion and a blade secured to opposite ends thereof, a pair of spaced apart bearing rings supporting each of said shafts in said casing, means locating each outermost bearing ring against radially outward displacement and spring means disposed intermediate each of said outermost bearing rings And a stepped portion of each stepped shaft whereby each of said blades is biased radially inwardly against said spherical surface.
Claim 2
Dependent Claim 160 words
In a gas turbine of the type having a high pressure turbine rotor, a low pressure turbine rotor and an intermediate annular guide ring disposed coaxially in a casing wherein said guide ring includes a plurality of blades each of which is mounted for rotation about an individual radially extending axis by means of a common gear ring disposed in meshing engagement with a pinion coaxially secured to each blade with each blade bearing on an inner spherical surface of said casing, the improvement comprising a plurality of stepped shaft means each having a pinion and a blade secured to opposite ends thereof, a pair of spaced apart bearing rings supporting each of said shafts in said casing, means locating each outermost bearing ring against radially outward displacement and spring means disposed intermediate each of said outermost bearing rings And a stepped portion of each stepped shaft whereby each of said blades is biased radially inwardly against said spherical surface.

References Cited (Backward Citations)

GB755527A Cited
GB878988A Cited
US3013771A Cited
US3574479A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-08-22 1976-02-21 1976-08-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-08-22 1980-02-21 1980-08-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-08-22 1984-02-21 1984-08-22 $7700.00 Window Closed / Lapsed

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