← Back to Patent Explorer
US4329644A Expired / Lapsed US ⏱️ 0.0 years remaining

Electrode structure for a high temperature capacitance probe for sensing turbine speed

Assignee: Honeywell International Inc
•
Filing: 1980-04-03
•
Granted: 1982-05-11
•
Expires: 2000-04-03
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A probe is constructed for placement in the hot turbine section of a gas turbine engine. A housing containing two electrodes extends through the turbine shroud into the tip clearance area of the turbine rotor. A voltage impressed across the electrodes will generate an electric field in the vicinity of the turbine blades which will be distorted as the blades pass, thereby generating a charge pulse at the output of the probe. The electrode conductors are imbedded in pins which are retained by insulating rings brazed in place. The electrodes extend slightly outward from the surrounding insulating surfaces to create an air gap around each electrode. This air gap provides additional insulation and prevents contamination.

Inventors

  • 👤 Zoltan L. Libertini
  • 👤 Alan R. Duly
  • 👤 Steven D. White

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 19:24
CPC Classifications
G; G01; G01B; G01B7/00; G01B7/14; F; F01; F01D; F01D17/00; F01D17/02; F01D17/06; F01D21/00; F01D21/04; G01P; G01P3/00; G01P3/42; G01P3/44; G01P3/48; G01P3/481; G01P3/483

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 241 words
A probe for sensing the passing of a rotor blade in the hot turbine section of a gas turbine engine comprising: a housing constructed of high temperature resistant material having an open receptacle constructed therein; an insulating member constructed of high temperature resistant insulating material secured in the receptacle of the housing and adapted to receive and position at least one pair of electrodes within the housing, said insulating member constructed to insulate the electrodes from the housing; at least one pair of electrodes constructed of high temperature resistant material mounted in locked position within the insulating member and further comprising: an electrode pin constructed to fit into the insulating member and being positioned thereby to extend outward from the housing; an electrode tip secured to the outer extremity of the electrode pin and extending transverse thereto to form an electrode having a substantially T-shaped cross section, said electrode tip being entirely surrounded by an air gap thereby increasing the over surface path between the electrodes and between the electrodes and the housing; a cable extending through the housing and containing a conductor connected to each electrode; and means to mount the probe in proximity to the turbine blades of the gas turbine engine in a position at which the electrodes extend into the turbine area sufficiently close to the turbine blades such that an electrical field applied to the electrodes will be altered by the passage of the turbine blades.
Claim 2
Dependent Claim 241 words
A probe for sensing the passing of a rotor blade in the hot turbine section of a gas turbine engine comprising: a housing constructed of high temperature resistant material having an open receptacle constructed therein; an insulating member constructed of high temperature resistant insulating material secured in the receptacle of the housing and adapted to receive and position at least one pair of electrodes within the housing, said insulating member constructed to insulate the electrodes from the housing; at least one pair of electrodes constructed of high temperature resistant material mounted in locked position within the insulating member and further comprising: an electrode pin constructed to fit into the insulating member and being positioned thereby to extend outward from the housing; an electrode tip secured to the outer extremity of the electrode pin and extending transverse thereto to form an electrode having a substantially T-shaped cross section, said electrode tip being entirely surrounded by an air gap thereby increasing the over surface path between the electrodes and between the electrodes and the housing; a cable extending through the housing and containing a conductor connected to each electrode; and means to mount the probe in proximity to the turbine blades of the gas turbine engine in a position at which the electrodes extend into the turbine area sufficiently close to the turbine blades such that an electrical field applied to the electrodes will be altered by the passage of the turbine blades.

References Cited (Backward Citations)

US2123812A Cited
US2653298A Cited
US2842738A Cited
US3714012A Cited
US4063167A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1985-05-10 1985-11-09 1986-05-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-05-10 1989-11-09 1990-05-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-05-10 1993-11-09 1994-05-11 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag