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US4820122A Expired / Lapsed US ⏱️ 0.0 years remaining

Dirt removal means for air cooled blades

Assignee: RTX Corp
•
Filing: 1988-04-25
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Granted: 1989-04-11
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Expires: 2008-04-25
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Abstract

Abstract Dirt removal means for an internally air cooled blade for a gas turbine engine of the type that includes multi passes some of which are serpentine as made in situ by casting the ribs so as to be angularly disposed at the root of the blade and a straight through passageway with an opening at the tip. The velocity of the airstream in the straight through passageway being sufficiently high to carry the dirt through the opening and the angularly disposed ribs overlying the entrance to the other passageway so as to divert the dirt entrained airstream into the straight through passageway while allowing relatively dirt-free air to turn the angle of the rib to enter the serpentine passes.

Inventors

  • 👤 Kenneth B. Hall
  • 👤 Thomas A. Auxier
  • 👤 Wesley D. Brown

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 18:43
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/32; F01D5/00; F01D5/12; F01D5/14; F01D5/18; F01D5/187; F05; F05D; F05D2260/00; F05D2260/60; F05D2260/607; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 145 words
An internally cooled blade for a gas turbine engine, said blade having a root section and tip section, wall means between said root section and tip section defining the airfoil of said blade, a plurality of ribs defining passageways extending spanwise in said blade for communicating cooling air through said blade discharging into the turbine engine's gas path through apertures formed in said airfoil, means for preventing dirt from clogging said apertures, said means including at least one straight through passageway and hole formed in said tip section sized for the largest particle of dirt anticipated to be entrained in said cooling air, and at least one rib at the root section having a baffle-like shaped portion angularly disposed relative to said passageways for directing the dirt entrained air into said straight through passageway and preventing said dirt entrained air from entering said other passageways.
Claim 2
Dependent Claim 145 words
An internally cooled blade for a gas turbine engine, said blade having a root section and tip section, wall means between said root section and tip section defining the airfoil of said blade, a plurality of ribs defining passageways extending spanwise in said blade for communicating cooling air through said blade discharging into the turbine engine's gas path through apertures formed in said airfoil, means for preventing dirt from clogging said apertures, said means including at least one straight through passageway and hole formed in said tip section sized for the largest particle of dirt anticipated to be entrained in said cooling air, and at least one rib at the root section having a baffle-like shaped portion angularly disposed relative to said passageways for directing the dirt entrained air into said straight through passageway and preventing said dirt entrained air from entering said other passageways.
Claim 3
Dependent Claim 16 words
An internally cooled blade as claimed in claim 1, wherein said blade is a turbine blade.
Claim 4
Dependent Claim 49 words
An internally cooled blade as claimed in claim 2, wherein the root of the blade includes additional ribs angularly disposed relative to the entrance to said passageways and spaced therefrom, at least one of said ribs being a portion of the wall defining at least one of said passageways.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-04-10 1992-10-10 1993-04-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-04-10 1996-10-10 1997-04-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-04-10 2000-10-10 2001-04-11 $7700.00 Window Closed / Lapsed

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