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Torence P Brogan

age ~54

from Anchorage, AK

Also known as:
  • Tory P Brogan
  • Porence P Brogan

Torence Brogan Phones & Addresses

  • Anchorage, AK
  • 130 Richmond Dr, Manchester, CT 06042 • 8604327510
  • Belgrade, MT
  • Port Saint Lucie, FL

Work

  • Position:
    Financial Professional

Education

  • Degree:
    Associate degree or higher

Us Patents

  • Augmentor Pilot

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  • US Patent:
    8209987, Jul 3, 2012
  • Filed:
    Nov 26, 2008
  • Appl. No.:
    12/323773
  • Inventors:
    Donald J. Hautman - Marlborough CT, US
    Jeffery A. Lovett - Tolland CT, US
    Torence P. Brogan - Manchester CT, US
  • Assignee:
    United Technologies Corporation - Hartford CT
  • International Classification:
    F02K 3/10
  • US Classification:
    60761
  • Abstract:
    A gas turbine engine augmenter has a gas flowpath. A number of vanes extend into the gas flowpath. A number of augmenter fuel conduits have outlets along at least some of the vanes. At least one burner discharge outlet is along at least one of the vanes for discharging a pilot gas.
  • Engine Hot Section Vane With Tapered Flame Holder Surface

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  • US Patent:
    8534071, Sep 17, 2013
  • Filed:
    Apr 6, 2012
  • Appl. No.:
    13/441031
  • Inventors:
    Jeffrey A. Lovett - Tolland CT, US
    Donald J. Hautman - Marlborough CT, US
    Torence P. Brogan - Manchester CT, US
    Christopher A. Eckett - New Britain CT, US
  • Assignee:
    United Technologies Corporation - Hartford CT
  • International Classification:
    F02K 3/10
  • US Classification:
    60765
  • Abstract:
    A gas turbine or rocket engine hot section includes a first duct case, a second duct case, a plurality of vanes arranged about an axial centerline, and an igniter located with a first of the plurality of vanes. The first of the plurality of vanes extends axially between a leading edge and a flame holder surface at a trailing edge. The flame holder surface extends radially between a first vane end connected to the first duct case and a second vane end connected to the second duct case. The flame holder surface includes a first section that tapers towards the first vane end, and a second section that tapers away from the first section and towards the second vane end.
  • Multi-Stage Amplification Vortex Mixture For Gas Turbine Engine Combustor

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  • US Patent:
    20130019604, Jan 24, 2013
  • Filed:
    Jul 21, 2011
  • Appl. No.:
    13/188451
  • Inventors:
    Frank J. Cunha - Avon CT, US
    Torence P. Brogan - Manchester CT, US
  • International Classification:
    F02C 7/00
  • US Classification:
    60772, 60737
  • Abstract:
    A multi-stage vortex mixer for a combustor of a gas turbine engine includes a vortex amplifier stage in communication with a first stage amplifier, the vortex amplifier stage in communication with a dilution hole.
  • Portable Self-Contained Telescoping Camera Tower System For High Angelimaging

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  • US Patent:
    57868549, Jul 28, 1998
  • Filed:
    Nov 21, 1995
  • Appl. No.:
    8/561371
  • Inventors:
    Mark W. Slade - Weston CT
    Veronia V. Slade - Weston CT
    Steven M. Nettik - Bozeman MT
    Torence P. Brogan - Belgrade MT
  • Assignee:
    Tree Top Systems, Inc. - Westport CT
  • International Classification:
    H04N 5225
    G03B 1700
  • US Classification:
    348373
  • Abstract:
    A portable, self-contained telescoping camera tower system permits high angle imaging and rapid and smooth change of perspective. The camera tower is a stand-alone unit capable of being transported, set up and operated by a single individual and which provides steady advance and retreat of the tower over its full range of up and down movement. An arrangement of pulleys, bearing surfaces, and drive means, preferably with two power-up drives and a separate power-down drive, assures smooth operation though its full operating range.

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