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Robert M Sonntag

from Bolton, CT
Age ~63
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Also known as:
Robert C Sonntag, Robert M Sountag, Rob M Sonntag, Rob'T C Sonntag, Robt C Sonntag, Bob M Sonntag
Phone and address:
8 Daria Dr, Manchester, CT 06043
(860) 649-6060
Related to:
Julia Tredinnick, 33
Connected to:
Adam J Sonntag, 38Alison H Sonntag, 77Anthony M Sonntag, 64Carla J Sonntag, 62Daris W Sonntag, 44Giovanni Sonntag, 45Gretchen J Sonntag, 73Jeff N Sonntag, 47Kim M Sonntag, 64Kristen M Sonntag, 50

Robert Sonntag Phones & Addresses

  • 8 Daria Dr, Bolton, CT 06043 (860) 649-6060
  • 42 Alexander St, Manchester, CT 06040 (860) 649-6060
  • 230 Locust Ln, Riverton, NJ 08077 (856) 829-5792
  • Cinnaminson, NJ
  • Jupiter, FL

Work

Position: Service Occupations

Education

Degree: Associate degree or higher

Professional Records

Medicine Doctors

Robert Sonntag Photo 1

Robert George Sonntag

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Specialties:
Internal Medicine
Geriatric Medicine
Hospice & Palliative Medicine
Family Medicine
Education:
University of Wisconsin at Madison (1975)

Publications

Us Patents

Thermal Barrier Coating

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US Patent:
7413808, Aug 19, 2008
Filed:
Oct 18, 2004
Appl. No.:
10/968322
Inventors:
Steven W. Burd - Cheshire CT, US
Robert M. Sonntag - Manchester CT, US
Kevin W. Schlichting - Storrs CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
B32B 9/00
US Classification:
428469, 428472, 428701, 428702, 416241 R, 416241 B
Abstract:
An article has a metallic substrate having a first emissivity. A thermal barrier coating atop the substrate may have an emissivity that is a substantial fraction of the first emissivity.

Thermal Barrier Coating

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US Patent:
8216687, Jul 10, 2012
Filed:
Mar 25, 2008
Appl. No.:
12/054801
Inventors:
Steven W. Burd - Cheshire CT, US
Robert M. Sonntag - Manchester CT, US
Kevin W. Schlichting - Storrs CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
B32B 9/00
B05D 1/36
US Classification:
428469, 428472, 4274192
Abstract:
An article has a metallic substrate having a first emissivity. A thermal barrier coating atop the substrate may have an emissivity that is a substantial fraction of the first emissivity.

Crack Resistant Combustor

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US Patent:
20090235666, Sep 24, 2009
Filed:
Mar 14, 2006
Appl. No.:
12/160226
Inventors:
Mark Edward Tuttle - Portland CT, US
Robert M. Sonntag - Manchester CT, US
John H. Nixon - Ellington CT, US
International Classification:
F23R 3/08
B23P 11/00
US Classification:
60752, 298892, 2989001
Abstract:
A combustion chamber louver assembly includes an aft louver having a forward panel that extends axially from a louver leading edge to a corner , and a forward louver joined to the forward panel of the aft louver. A lip defined by a portion of the forward louver that extends axially past the corner to a louver trailing edge includes circumferentially distributed trailing edge slots extending forwardly from the trailing edge a nominal distance equal to about 88% to 95% of the length L of the lip.

Cooled Gas Turbine Stator Assembly

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US Patent:
20100303610, Dec 2, 2010
Filed:
May 29, 2009
Appl. No.:
12/474822
Inventors:
William A. Daniels - Marlborough CT, US
Robert M. Sonntag - Bolton CT, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F01D 25/12
F01D 9/02
US Classification:
415115
Abstract:
A stator assembly for a gas turbine engine is provided having an annular body, an inner gas path platform, a plurality of fairings, and at least one nozzle. The annular body has an outer gas path platform and a circumferentially extending annular cavity disposed radially outside of the outer gas path platform. The fairings extend radially between the inner gas path platform and the outer gas path platform. Each fairing includes a gas passage extending from the annular cavity through the inner gas path platform. The at least one nozzle has an inlet orifice disposed outside of the annular cavity and an exit orifice disposed within the annular cavity. The exit orifice is oriented within the annular cavity such that cooling air exiting the nozzle travels in a substantially circumferential direction within the annular cavity.

Heat Shield For A Combustor

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US Patent:
20130192233, Aug 1, 2013
Filed:
Feb 17, 2012
Appl. No.:
13/399399
Inventors:
Jonathan Jeffery Eastwood - Newington CT, US
Joey Wong - Enfield CT, US
Robert M. Sonntag - Bolton CT, US
Albert K. Cheung - East Hampton CT, US
Timothy S. Snyder - Glastonbury CT, US
International Classification:
F23R 3/42
F23R 3/00
US Classification:
60752
Abstract:
A heat shield includes a panel having a forward face and an aft face, a circumferential outer side and a circumferential inner side such that the panel subtends a predetermined arc, and a first radially extending side and a second radially extending side each extending from the circumferential outer side to the circumferential inner side. The panel defines an opening extending between the forward face and the aft face, a lip projecting from the forward face and extending around the opening, a rail projecting from the forward face and extending around the lip to define a cavity region between the lip and the rail, and a plurality of holes in the cavity region. Each of the plurality of holes extends from the forward face to the aft face. A region of the panel extending from the lip to the circumferential outer side is free of any aft-projecting features.

Annular Combustor

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US Patent:
20130192262, Aug 1, 2013
Filed:
Feb 17, 2012
Appl. No.:
13/399442
Inventors:
Jonathan Jeffery Eastwood - Newington CT, US
Joey Wong - Enfield CT, US
Robert M. Sonntag - Bolton CT, US
International Classification:
F23R 3/00
B23P 15/00
B23P 11/02
F02C 3/04
US Classification:
60805, 60722, 29428, 29447
Abstract:
An annular combustor includes an annular outer shell that includes a first flange that defines an inner diameter IDand an annular inner shell that includes a second flange that defines an outer diameter OD. An annular hood includes a radially outer hood flange and a radially inner hood flange. A bulkhead includes a radially outer bulkhead flange that defines an outer diameter ODand a radially inner bulkhead flange that defines an inner diameter ID. The first flange is secured at a radially outer joint between the radially outer hood flange and the radially outer bulkhead flange. The second flange is secured at a radially inner joint between the radially inner hood flange and the radially inner bulkhead flange. The IDand the ODdefine a ratio R1 of ID/ODthat is 0.998622-1.001129, and the IDand the ODdefine a ratio R2 of ID/ODthat is 0.998812-1.001388.

Fuel Distribution Within A Gas Turbine Engine Combustor

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US Patent:
20130199200, Aug 8, 2013
Filed:
Mar 15, 2013
Appl. No.:
13/832507
Inventors:
UNITED TECHNOLOGIES CORPORATION - Hartford CT, US
Timothy S. Snyder - Glastonbury CT, US
David Kwoka - South Glastonbury CT, US
Robert M. Sonntag - Bolton CT, US
Assignee:
UNITED TECHNOLOGIES CORPORATION - Hartford CT
International Classification:
F02C 7/22
US Classification:
60776, 60739
Abstract:
A fuel system for a gas turbine engine includes a plurality of duplex nozzles arranged on each side of top dead center and a plurality of simplex nozzles. A primary manifold is operable to communicate fuel to a primary flow jet in each of the plurality of duplex nozzles and a secondary manifold is operable to communicate fuel to a secondary flow jet in each of the plurality of duplex nozzles and a secondary flow jet in each of the plurality of simplex nozzles. An equalizer valve that is in communication with both the primary manifold and the secondary manifold distributes fuel at various pressures to both the primary and secondary manifolds.

Turbine Engine Combustor Wall With Non-Uniform Distribution Of Effusion Apertures

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US Patent:
20130340437, Dec 26, 2013
Filed:
Jun 22, 2012
Appl. No.:
13/531132
Inventors:
Nurhak Erbas-Sen - Manchester CT, US
James B. Hoke - Tolland CT, US
Albert K. Cheung - East Hampton CT, US
Robert M. Sonntag - Bolton CT, US
Timothy S. Snyder - Glastonbury CT, US
Assignee:
UNITED TECHNOLOGIES CORPORATION - Hartford CT
International Classification:
F23R 3/02
F02C 3/00
US Classification:
60754
Abstract:
A turbine engine combustor wall includes support shell and a heat shield. The support shell includes shell quench apertures, first impingement apertures, and second impingement apertures. The combustor heat shield includes shield quench apertures fluidly coupled with the shell quench apertures, first effusion apertures fluidly coupled with the first impingement apertures, and second effusion apertures fluidly coupled with the second impingement apertures. The shield quench apertures and the first effusion apertures are configured in a first axial region of the heat shield, and the second effusion apertures are configured in a second axial region of the heat shield located axially between the first axial region and a downstream end of the heat shield. A density of the first effusion apertures in the first axial region is greater than a density of the second effusion apertures in the second axial region.

Isbn (Books And Publications)

Structures/How Businesses, Entrepreneurs, and the Free Market Work, a Guide for the 58% of Americans Who Dream of Owning Their Own Businesses!

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Author

Robert E. Sonntag

ISBN #

0938545000

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Robert M Sonntag from Bolton, CT, age ~63 Get Report