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Anita L Tracy

from Middletown, CT
Age ~57

Anita Tracy Phones & Addresses

  • 93 Spring Brook Dr, Middletown, CT 06457 (860) 344-1580
  • 3 Town Colony Dr, Middletown, CT 06457 (860) 635-1346
  • 138 Town Colony Dr, Middletown, CT 06457
  • 1403 14Th Ct, Jupiter, FL 33477 (561) 776-6314
  • East Hartford, CT
  • Roslindale, MA
  • College Park, MD
  • West Palm Beach, FL
  • Millersville, MD

Work

Position: Machine Operators, Assemblers, and Inspectors Occupations

Education

Degree: Bachelor's degree or higher

Business Records

Name / Title
Company / Classification
Phones & Addresses
Anita Tracy
CONNECTICUT BETA OF PI BETA PHI HOUSE CORPORATION
85 Montowese Trl, Wallingford, CT 06492
90 Sring St, Middletown, CT 06457
90 Spg St, Middletown, CT 06457

Publications

Us Patents

Turbine Airfoil With Platform Cooling

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US Patent:
20090116953, May 7, 2009
Filed:
Nov 2, 2007
Appl. No.:
11/982578
Inventors:
Brandon W. Spangler - Vernon CT, US
Corneil S. Paauwe - Manchester CT, US
Christopher J. Lehane - South Windsor CT, US
Anita L. Tracy - Middletown CT, US
John D. Wiedemer - Glastonbury CT, US
Scott D. Hjelm - Windsor Locks CT, US
International Classification:
F02C 7/18
F02C 7/28
US Classification:
415115, 415116
Abstract:
Convective cooling of gas turbine engine airfoil platforms is enhanced by grooving the interface of the platforms with corresponding platform-to-platform seals, thereby accelerating cooling airflow over the platform surfaces.

Airfoil With Break-Way, Free-Floating Damper Member

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US Patent:
20130276455, Oct 24, 2013
Filed:
Apr 24, 2012
Appl. No.:
13/454183
Inventors:
Benjamin T. Fisk - East Granby CT, US
Gregory M. Dolansky - Higganum CT, US
David P. Houston - Glastonbury CT, US
Anita L. Tracy - Middletown CT, US
International Classification:
F01D 5/16
B05D 1/36
F02C 3/04
US Classification:
60805, 416145, 427180
Abstract:
An airfoil includes an airfoil body that has a leading edge and a trailing edge and a first sidewall and a second sidewall that is spaced apart from the first sidewall. The first sidewall and the second sidewall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. A damper member is enclosed in the cavity and is free-floating within the cavity.

Airfoil Including Member Connected By Articulated Joint

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US Patent:
20130276456, Oct 24, 2013
Filed:
Apr 24, 2012
Appl. No.:
13/454204
Inventors:
Anita L. Tracy - Middletown CT, US
International Classification:
F01D 5/14
B21D 53/78
F02C 3/04
US Classification:
60805, 416239, 29889
Abstract:
An airfoil includes a body that has a platform, an airfoil extending outwardly from a side of the platform and a root extending outwardly from another side of the platform. A member is connected in an articulated joint to the body.

Airfoil Including Loose Damper

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US Patent:
20130276457, Oct 24, 2013
Filed:
Apr 24, 2012
Appl. No.:
13/454488
Inventors:
David P. Houston - Glastonbury CT, US
Benjamin T. Fisk - East Granby CT, US
Anita L. Tracy - Middletown CT, US
International Classification:
F01D 5/16
F02C 3/04
US Classification:
60805, 416232
Abstract:
An airfoil includes an airfoil body that has a leading edge and a trailing edge and a first sidewall and a second sidewall that is spaced apart from the first sidewall. The first sidewall and the second sidewall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. A damper member is enclosed in the cavity and is loose within the cavity.

Airfoil Having Minimum Distance Ribs

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US Patent:
20130276460, Oct 24, 2013
Filed:
Apr 24, 2012
Appl. No.:
13/454253
Inventors:
Benjamin T. Fisk - East Granby CT, US
Steven Taffet - South Windsor CT, US
Gregory M. Dolansky - Higganum CT, US
Anita L. Tracy - Middletown CT, US
International Classification:
F01D 5/14
B23P 15/02
F02C 3/06
US Classification:
60806, 416236 R, 298897
Abstract:
An airfoil includes an airfoil body that defines a longitudinal axis. The airfoil body includes a leading edge and a trailing edge and a first side wall and a second side wall that is spaced apart from the first side wall to define a camber line there between. The first side wall and the second side wall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. Multiple ribs extend longitudinally in the cavity and are laterally spaced apart from each other relative to the longitudinal axis. In at least one plane that is perpendicular to the longitudinal axis, each of the ribs connects the first side wall and the second side wall along respective minimum distance directions that are perpendicular to the camber line. At least two of the respective minimum distance directions are non-parallel.

Airfoil Having Internal Lattice Network

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US Patent:
20130276461, Oct 24, 2013
Filed:
Apr 24, 2012
Appl. No.:
13/454283
Inventors:
Sergio M. Loureiro - Glastonbury CT, US
Agnes Klucha - Colchester CT, US
Benjamin T. Fisk - East Granby CT, US
Anita L. Tracy - Middletown CT, US
International Classification:
F01D 5/18
F02C 3/04
F01D 5/14
US Classification:
60806, 416227 R
Abstract:
An airfoil includes an airfoil body that defines a longitudinal axis. The airfoil body includes a leading edge and a trailing edge and a first side wall and a second side wall that is spaced apart from the first side wall. The first side wall and the second side wall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. A lattice network connects the first side and the second side. The lattice network includes at least one enlarged node spaced apart from the first side wall and the second side wall and ribs that extend from the at least one enlarged node. Each of the ribs connects to one of the first side wall and the second side wall.

Airfoil Having Tapered Butress

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US Patent:
20130280059, Oct 24, 2013
Filed:
Apr 24, 2012
Appl. No.:
13/454369
Inventors:
Gregory M. Dolansky - Higganum CT, US
Benjamin T. Fisk - East Granby CT, US
Anita L. Tracy - Middletown CT, US
International Classification:
F03B 11/02
US Classification:
4152081
Abstract:
An airfoil includes an airfoil body that defines a longitudinal axis. The airfoil body includes a leading edge and a trailing edge and a first side wall and a second side wall that is spaced apart from the first sidewall. The first side wall and the second side wall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. At least one of the first side wall and the second side wall includes at least one longitudinally elongated buttress that tapers longitudinally. The at least one longitudinally elongated buttress defines an increased thickness of, respectively, the first side wall or the second sidewall. The at least one longitudinally elongated buttress projects partially across the cavity toward the other of the first side wall or the second sidewall.

Airfoil Support Method And Apparatus

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US Patent:
20130280074, Oct 24, 2013
Filed:
Apr 24, 2012
Appl. No.:
13/454599
Inventors:
David P. Houston - Glastonbury CT, US
Anita L. Tracy - Middletown CT, US
International Classification:
F04D 29/34
B23P 15/00
US Classification:
416204 R, 2988802
Abstract:
A support for an airfoil includes a trunk and a limb extending from the trunk for distribution within the airfoil.
Anita L Tracy from Middletown, CT, age ~57 Get Report