Philip J Kirsopp

age ~49

from Lebanon, CT

Also known as:
  • Philip James Kirsopp
  • Philip Kirsopp
  • Phillip Kirsopp
  • Phil Kirsopp
  • James Kirsopp
  • Kirsopp Kirsopp
Phone and address:
214 Mack Rd, Exeter, CT 06249
8606421819

Philip Kirsopp Phones & Addresses

  • 214 Mack Rd, Lebanon, CT 06249 • 8606421819
  • 61 Old Town Rd, Ashford, CT 06278 • 8604295141
  • 13104 154Th Rd, Jupiter, FL 33478 • 5617441683
  • 13310 170Th Rd N, Jupiter, FL 33478 • 8606421819
  • 2840 Parrish Cemetery Rd, Jacksonville, FL 32221
  • 11705 Wattle Tree Rd, Jacksonville, FL 32246 • 9046426119 • 8606421819
  • 64 Cypress Pond Rd, Port Orange, FL 32124 • 8606421819
  • Daytona Beach, FL
  • Palm Beach, FL

Industries

Aviation & Aerospace

Resumes

Philip Kirsopp Photo 1

Ngpf 30K Combustor/Fuel Nozzle Ipt Leader

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Location:
Hartford, Connecticut Area
Industry:
Aviation & Aerospace

Us Patents

  • Fuel Injector Bearing Plate Assembly And Swirler Assembly

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  • US Patent:
    8291706, Oct 23, 2012
  • Filed:
    Jun 11, 2009
  • Appl. No.:
    12/482516
  • Inventors:
    Keith M. Tanner - Colchester CT, US
    Philip J. Kirsopp - Lebanon CT, US
  • Assignee:
    United Technologies Corporation - Hartford CT
  • International Classification:
    F02C 1/00
    F02G 3/00
  • US Classification:
    60740, 60737, 60800, 60796, 2395871
  • Abstract:
    A bearing plate assembly for a turbine engine fuel injector includes a bearing plate , with an opening bordered by a race. A swivel ball nests inside the race and is rotatable relative thereto. A lock, which may be a tip bushing resists disengagement of the swivel ball from the race. A fuel injector nozzle extends through an opening in the swivel ball. During engine operation, the ball can swivel inside the race to accommodate rotational movement of the nozzle about lateral and radial axes.
  • Fuel Injector Bearing Plate Assembly And Swirler Assembly

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  • US Patent:
    20060207258, Sep 21, 2006
  • Filed:
    Mar 21, 2005
  • Appl. No.:
    11/085493
  • Inventors:
    Keith Tanner - Colchester CT, US
    Philip Kirsopp - Lebanon CT, US
  • International Classification:
    F23R 3/14
  • US Classification:
    060748000, 060740000
  • Abstract:
    A bearing plate assembly for a turbine engine fuel injector includes a bearing plate , with an opening bordered by a race . A swivel ball nests inside the race and is rotatable relative thereto. A lock, which may be a tip bushing resists disengagement of the swivel ball from the race. A fuel injector nozzle extends through an opening in the swivel ball. During engine operation, the ball can swivel inside the race to accommodate rotational movement of the nozzle about lateral and radial axes.
  • Combustor Turbine Interface For A Gas Turbine Engine

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  • US Patent:
    20110052381, Mar 3, 2011
  • Filed:
    Aug 28, 2009
  • Appl. No.:
    12/549693
  • Inventors:
    James B. Hoke - Tolland CT, US
    Philip J. Kirsopp - Lebanon CT, US
  • International Classification:
    F01D 9/04
  • US Classification:
    415191
  • Abstract:
    A turbine vane downstream of a combustor section includes an arcuate outer vane platform defined about an axis, the arcuate outer vane platform includes a segment of the arcuate outer vane platform along the axis which follows an outer combustor liner panel structure and an arcuate inner vane platform defined about the axis, the arcuate inner vane platform includes a segment of the arcuate inner vane platform along the axis which follows an inner combustor liner panel structure.
  • Combustor Panel Arrangement

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  • US Patent:
    20110126543, Jun 2, 2011
  • Filed:
    Nov 30, 2009
  • Appl. No.:
    12/627528
  • Inventors:
    Philip J. Kirsopp - Lebanon CT, US
    Aaron J. Dornback - Wethersfield CT, US
    James B. Hoke - Tolland CT, US
  • Assignee:
    United Technologies Corporation - Hartford CT
  • International Classification:
    F02C 7/22
    F02C 3/14
  • US Classification:
    60742, 60754
  • Abstract:
    A combustor module for a gas turbine engine is provided that includes a first annular liner assembly extending along a longitudinal axis of the engine. The first annular liner assembly includes a first annular support shell and a plurality of first heat shield panels coupled to the first annular support shell. The first heat shield panels form a segmented ring defining a plurality of first axial seams therebetween. The combustor module further includes a bulkhead coupled to the first annular liner assembly. The bulkhead provides a plurality of fuel nozzles for passing a first mass flow comprising fuel and air. The combustor module further includes a second annular liner assembly coupled to the bulkhead. The second annular liner assembly is in spaced-apart generally coaxial relationship from the first annular liner assembly by a channel height H. The second annular liner assembly includes an air admittance hole having a mean diameter D extending along a hole axis. The hole axis is offset from the first axial seam defined by the first heat shield panels.
  • Fuel Injector Bearing Plate Assembly And Swirler Assembly

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  • US Patent:
    20130341912, Dec 26, 2013
  • Filed:
    Jun 11, 2009
  • Appl. No.:
    12/482513
  • Inventors:
    Keith M. Tanner - Colchester CT, US
    Philip J. Kirsopp - Lebanon CT, US
  • International Classification:
    F23R 3/28
    F16L 27/08
  • US Classification:
    285272, 384 2
  • Abstract:
    A bearing plate assembly for a turbine engine fuel injector includes a bearing plate with an opening bordered by a race A swivel ball nests inside the race and is rotatable relative thereto. A lock, which may be a tip bushing resists disengagement of the swivel ball from the race. A fuel injector nozzle extends through an opening in the swivel ball. During engine operation, the ball can swivel inside the race to accommodate rotational movement of the nozzle about lateral and radial axes.

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Philip Kirsopp Ashford C...

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Philip Kirsopp

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Philip Kirsopp

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