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US5151325A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of dynamically balancing ceramic turbine wheels

Assignee: Honeywell International Inc
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Filing: 1990-12-11
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Granted: 1992-09-29
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Expires: 2010-12-11
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Abstract

Abstract Ceramic turbine wheels are balanced to minimize rotational vibrations by bonding silica-based glass pads to the wheel. The pads are formed from a mixture of sodium silicate, water and a fine ceramic powder, preferably of a composition similar to the underlying ceramic turbine wheel. The weighted pads are machined, without damage to the underlying ceramic wheel, to achieve proper balance.

Inventors

  • 👤 Barry S. Draskovich

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 21:07
CPC Classifications
C; C04; C04B; C04B35/00; C04B35/622; C04B35/626; C04B35/63; C04B35/6303; C04B35/6316; F; F01; F01D; F01D5/00; F01D5/02; F01D5/027; F16; F16F; F16F15/00; F16F15/32; Y; Y10; Y10T; Y10T428/00; Y10T428/25; Y10T428/252; Y10T428/30

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 32 words
In a gas turbine engine, a ceramic turbine wheel having thereon a glassy balancing pad formed from a cured mixture of a fine powder of said ceramic in a sodium silicate solution.
Claim 2
Dependent Claim 32 words
In a gas turbine engine, a ceramic turbine wheel having thereon a glassy balancing pad formed from a cured mixture of a fine powder of said ceramic in a sodium silicate solution.
Claim 3
Dependent Claim 110 words
In gas turbomachinery, a dynamically balanced, silicon-containing ceramic wheel selected from the group consisting of silicon carbide and silicon coated carbon-carbon composites, said wheel balanced by a method comprising the steps of: predetermining the location and amount of additional mass needed to balance said wheel, preparing a mixture of -325 mesh size silicon carbide powder and sodium silicate solution, applying a thin layer of said mixture to the wheel at said predetermined location, allowing said mixture to solidify, applying sufficient additional layers of said mixture to add about said predetermined amount of additional mass to the wheel, and curing said mixture before using said wheel in a gas turbine engine.
Claim 4
Dependent Claim 110 words
In gas turbomachinery, a dynamically balanced, silicon-containing ceramic wheel selected from the group consisting of silicon carbide and silicon coated carbon-carbon composites, said wheel balanced by a method comprising the steps of: predetermining the location and amount of additional mass needed to balance said wheel, preparing a mixture of -325 mesh size silicon carbide powder and sodium silicate solution, applying a thin layer of said mixture to the wheel at said predetermined location, allowing said mixture to solidify, applying sufficient additional layers of said mixture to add about said predetermined amount of additional mass to the wheel, and curing said mixture before using said wheel in a gas turbine engine.
Claim 5
Dependent Claim 99 words
A gas turbine engine having a dynamically balanced, silicon-containing ceramic wheel balanced by a method comprising the steps of: predetermining the location and amount of additional mass needed to balance said wheel, preparing a mixture of fine ceramic powder and sodium silicate solution, applying a thin layer of said mixture to the wheel at said predetermined location, allowing said mixture to solidify, applying sufficient additional layers of said mixture to add, in total, more than said predetermined amount of additional mass to the wheel, curing said mixture; and machining away the excess mass of mixture to balance the wheel.
Claim 6
Dependent Claim 99 words
A gas turbine engine having a dynamically balanced, silicon-containing ceramic wheel balanced by a method comprising the steps of: predetermining the location and amount of additional mass needed to balance said wheel, preparing a mixture of fine ceramic powder and sodium silicate solution, applying a thin layer of said mixture to the wheel at said predetermined location, allowing said mixture to solidify, applying sufficient additional layers of said mixture to add, in total, more than said predetermined amount of additional mass to the wheel, curing said mixture; and machining away the excess mass of mixture to balance the wheel.
Claim 7
Dependent Claim 66 words
In a gas turbine engine, a dynamically balanced, silicon carbide turbine wheel balanced by a method comprising: applying to the wheel a balancing composition solution consisting essentially of about equal parts by weight of -325 mesh size silicon carbide powder and sodium silicate, curing the composition to a solid mass, and adjusting the amount of balancing composition on the wheel to achieve the desired dynamic balance.
Claim 8
Dependent Claim 66 words
In a gas turbine engine, a dynamically balanced, silicon carbide turbine wheel balanced by a method comprising: applying to the wheel a balancing composition solution consisting essentially of about equal parts by weight of -325 mesh size silicon carbide powder and sodium silicate, curing the composition to a solid mass, and adjusting the amount of balancing composition on the wheel to achieve the desired dynamic balance.
Claim 9
Dependent Claim 58 words
In gas turbomachinery, a dynamically balanced, silicon nitride turbine wheel balanced by a method comprising: applying to the wheel a balancing composition consisting essentially of a fine silicon nitride powder in a sodium silicate solution, curing the composition to a solid mass, and adjusting the amount of balancing composition on the wheel to achieve the desired dynamic balance.
Claim 10
Dependent Claim 58 words
In gas turbomachinery, a dynamically balanced, silicon nitride turbine wheel balanced by a method comprising: applying to the wheel a balancing composition consisting essentially of a fine silicon nitride powder in a sodium silicate solution, curing the composition to a solid mass, and adjusting the amount of balancing composition on the wheel to achieve the desired dynamic balance.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-09-29 1996-03-30 1996-09-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-09-29 2000-03-30 2000-09-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-09-29 2004-03-30 2004-09-29 $7700.00 Window Closed / Lapsed

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