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US4247249A Expired / Lapsed US ⏱️ 0.0 years remaining

Turbine engine shroud

Assignee: General Electric Co
•
Filing: 1978-09-22
•
Granted: 1981-01-27
•
Expires: 1998-09-22
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Abstract

Abstract High temperature resistant turbine engine shrouds are formed of an amphoteric refractory oxide, a phosphate binding agent and optionally a stabilizer, reinforcement and/or porosity controller.

Inventors

  • 👤 Paul A. Siemers

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 21:21
CPC Classifications
F; F01; F01D; F01D11/00; F01D11/08; F01D11/12; F01D11/122; Y; Y02; Y02T; Y02T50/00; Y02T50/60; Y10; Y10S; Y10S277/00; Y10S277/935; Y10S277/939; Y10S277/941; Y10S277/943; Y10S60/00; Y10S60/909

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 129 words
In a gas turbine engine, a shroud comprising a plurality of arcuate segments disposed in end to end relationship to surround the tips of the rotor blades of the engine wherein each segment has a sealing surface which opposes the tips of the blades wherein the sealing surface is formed of an amphoteric refractory oxide matrix of material selected from ZrO 2 , Al 2 O 3 , Ce 2 O, ThO 2 and HfO 2 or mixture, a phosphate binding agent stable above about 1350° C., and from 0 to 50% by weight of the matrix material of a stabilizer selected from Y 2 O 3 , MgO, CaO, rare earth oxide or mixture and from 0 to 25% by weight of the matrix material of a filler.
Claim 2
Dependent Claim 129 words
In a gas turbine engine, a shroud comprising a plurality of arcuate segments disposed in end to end relationship to surround the tips of the rotor blades of the engine wherein each segment has a sealing surface which opposes the tips of the blades wherein the sealing surface is formed of an amphoteric refractory oxide matrix of material selected from ZrO 2 , Al 2 O 3 , Ce 2 O, ThO 2 and HfO 2 or mixture, a phosphate binding agent stable above about 1350° C., and from 0 to 50% by weight of the matrix material of a stabilizer selected from Y 2 O 3 , MgO, CaO, rare earth oxide or mixture and from 0 to 25% by weight of the matrix material of a filler.
Claim 3
Dependent Claim 14 words
The shroud of claim 1 wherein the amphoteric refractory oxide is ZrO 2 .
Claim 4
Dependent Claim 21 words
The shroud of claim 2 wherein from 4 to 50% of a stabilizer is employed of Y 2 O 3 .
Claim 5
Dependent Claim 21 words
The shroud of claim 1 wherein a mixture of phosphate is employed of H 3 PO 4 and AlPO 4 .
Claim 6
Dependent Claim 26 words
The shroud of claim 1 wherein a filler is employed of up to 25% of the matrix material selected from graphite, silicon carbide whisker and mixtures.
Claim 7
Dependent Claim 34 words
The shroud of claim 1 wherein the matrix material is selected from ZrO 2 , HfO 2 and mixtures and the stabilizer is selected from Y 2 O 3 , MgO, CaO and mixtures.
Claim 8
Dependent Claim 29 words
The shroud of claim 1 wherein the sealing surface is formed of ZrO 2 stabilized with Y 2 O 3 , H 3 PO 4 and silicon carbide whiskers.

References Cited (Backward Citations)

US3879831A Cited
US3843400A Cited
US4087199A Cited
US4128433A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-01-27 1984-07-28 1985-01-27 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-01-27 1988-07-28 1989-01-27 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-01-27 1992-07-28 1993-01-27 $7700.00 Window Closed / Lapsed

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