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US3383091A Expired / Lapsed US ⏱️ 0.0 years remaining

Radial turbine blade damping device

Assignee: Pratt and Whitney Canada Corp
•
Filing: 1966-07-21
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Granted: 1968-05-14
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Expires: 1986-07-21
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Abstract

No abstract record available.

Inventors

  • 👤 Newland Allan Burrell

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 20:03
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/02; F01D5/04; F01D5/043; F01D5/045; Y; Y10; Y10S; Y10S416/00; Y10S416/50

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 151 words
IN A CENTRIPETAL HIGH VELOCITY GAS TURBINE WHEEL HAVING AN AXIS OF ROTATION, AXIALLY SEPARATE LEADING AN EXDUCER WHEEL SECTIONS, EACH SAID SECTION HAVING A HUB AND BLADES EXTENDING RADIALLY FROM THE HUB, AND THE HUBS BEING INTERCONNECTED FOR SIMULTANEOUS ROTATION, AND THE LEADING AND EXDUCER BLADES HAVING RESPECTIVE ADJACENT EDGES ALIGNED, THE IMPROVEMENT IN WHICH THE ADJACENT EDGES OF EACH ONE OF LEADING BLADE AND ALIGNED EXDUCER BLADE COMPRISE: RECESSED PORTIONS EXTENDING OVER PART OF THEIR RADIAL LENGTH, THE RECESSES PROVIDING AXIAL SEPARATION OF SAID PORTIONS OF THE EDGES, AND REMAINING PORTIONS WHICH ARE OUTWARDLY PROJECTED FROM THE SAID RECESSED PORTIONS AND WHICH ABUT IN A PLANE WHICH IN ONE DIMENSION IS RADIAL AND IN THE OTHER DIMENSION IS OBLIQUE TO THE PLANE OF THE BLADES IN SAID REGION, SAID OBLIQUE PLANE BEING DIRECTED OPPOSITELY WITH RESPECT TO SAID PLANE OF THE BLADES IN EACH PAIR OF CIRCUMFERENTIALLY ADJACENT BLADES.
Claim 2
Dependent Claim 151 words
IN A CENTRIPETAL HIGH VELOCITY GAS TURBINE WHEEL HAVING AN AXIS OF ROTATION, AXIALLY SEPARATE LEADING AN EXDUCER WHEEL SECTIONS, EACH SAID SECTION HAVING A HUB AND BLADES EXTENDING RADIALLY FROM THE HUB, AND THE HUBS BEING INTERCONNECTED FOR SIMULTANEOUS ROTATION, AND THE LEADING AND EXDUCER BLADES HAVING RESPECTIVE ADJACENT EDGES ALIGNED, THE IMPROVEMENT IN WHICH THE ADJACENT EDGES OF EACH ONE OF LEADING BLADE AND ALIGNED EXDUCER BLADE COMPRISE: RECESSED PORTIONS EXTENDING OVER PART OF THEIR RADIAL LENGTH, THE RECESSES PROVIDING AXIAL SEPARATION OF SAID PORTIONS OF THE EDGES, AND REMAINING PORTIONS WHICH ARE OUTWARDLY PROJECTED FROM THE SAID RECESSED PORTIONS AND WHICH ABUT IN A PLANE WHICH IN ONE DIMENSION IS RADIAL AND IN THE OTHER DIMENSION IS OBLIQUE TO THE PLANE OF THE BLADES IN SAID REGION, SAID OBLIQUE PLANE BEING DIRECTED OPPOSITELY WITH RESPECT TO SAID PLANE OF THE BLADES IN EACH PAIR OF CIRCUMFERENTIALLY ADJACENT BLADES.

References Cited (Backward Citations)

US2405283A Cited
US2941780A Cited
US3167301A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1971-05-14 1971-11-13 1972-05-14 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1975-05-14 1975-11-13 1976-05-14 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1979-05-14 1979-11-13 1980-05-14 $7700.00 Window Closed / Lapsed

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