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Thomas Milidantri Phones & Addresses

  • 136 Spring St, Goshen, NY 10924 (845) 294-3234
  • Jensen Beach, FL
  • West Palm Beach, FL
  • 45 Schreiber St, Tappan, NY 10983 (845) 398-0986
  • 385 Washington St, Tappan, NY 10983 (845) 398-0718 (845) 398-0986
  • 393 Washington St, Tappan, NY 10983 (845) 398-0986
  • Airmont, NY
  • Blauvelt, NY

Business Records

Name / Title
Company / Classification
Phones & Addresses
Thomas Milidantri
Manager Process Improvement
ChromaScape, Inc.
Chemicals · Renewables & Environment · Mfg Aircraft Engines/Parts · Manufacturing - Colorants · Mfg Wood Products · Nonclassifiable Establishments · Mfg Turbines/Generator Sets · Mfg Aircraft Engine/Part Repair Services Airport/Airport Services
2055 Enterprise Pkwy, Twinsburg, OH 44087
330 Blaisdell Rd, Orangeburg, NY 10962
300 Blaisdell Rd, Orangeburg, NY 10962
2390 E Camelback Rd, Phoenix, AZ 85016
(845) 359-4700, (330) 425-4244, (914) 359-2462

Publications

Us Patents

Turbine Component Fixture For Manufacture Or Repair

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US Patent:
20060085978, Apr 27, 2006
Filed:
Oct 21, 2004
Appl. No.:
10/970560
Inventors:
Thomas Milidantri - Goshen NY, US
International Classification:
B23P 6/00
US Classification:
029889100, 029402010, 029402190, 029889200, 029889230
Abstract:
A process is provided for manufacturing or repairing a turbine component, wherein the component has an internal cavity open to the outside, by inserting into the internal cavity a part of a fixture, with the part secured to the internal surface of the internal cavity of the component to hold the component and carrying out a manufacturing or repair process on an exterior surface of the turbine component.

Repair Of A Shrouded Blade

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US Patent:
20140003948, Jan 2, 2014
Filed:
Jun 14, 2013
Appl. No.:
13/917876
Inventors:
Gregory Alan Dubs - Palm Beach Gardens FL, US
Thomas Horace Milidantri - Jensen Beach FL, US
International Classification:
F01D 5/00
US Classification:
416189, 298891
Abstract:
The present invention discloses a novel and improved method for repairing a shrouded blade and a reconditioned shrouded blade. More specifically, a way of measuring a set of previously-operated blades to determine their post-operation geometric characteristics is provided where an offset due to deformation of the hardface surfaces of the shroud is determined. The hardface surfaces of the shroud are rough-machined and blade-compatible material is added to the hardface surfaces. A first side hardface surface of the shroud is then machined to a desired dimension offset relative to an originally manufactured blade after which a second side hardface surface is machined such that the distance between the hardface surfaces satisfies the cross-shroud dimension, which is similar to that of an originally manufactured blade.

Welding High-Strength Nickel Base Superalloys

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US Patent:
51060108, Apr 21, 1992
Filed:
Sep 28, 1990
Appl. No.:
7/590220
Inventors:
Richard J. Stueber - Suffern NY
Thomas Milidantri - Monsey NY
Moshen Tadayon - Washingtonville NY
Assignee:
Chromalloy Gas Turbine Corporation - Orangeburg NY
International Classification:
B23K 3102
US Classification:
228232
Abstract:
A process is provided for welding a gamma-prime precipitation-strengthened nickel base superalloy by heating the weld area and adjacent region to a ductile temperature, welding while maintaining the entire weld area and adjacent region at the ductile temperature and holding the weldment, weld area and adjacent region at the ductile temperature until the entire weld has solidified. The ductile temperature is above the aging temperature but below the incipient melting temperatures of the superalloy.

Welding High-Strength Nickel Base Superalloys

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US Patent:
53743199, Dec 20, 1994
Filed:
Nov 4, 1991
Appl. No.:
7/787546
Inventors:
Richard J. Stueber - Suffern NY
Thomas Milidantri - Monsey NY
Moshen Tadayon - Washingtonville NY
Assignee:
Chromalloy Gas Turbine Corporation - Orangeburg NY
International Classification:
C22C 2706
US Classification:
148404
Abstract:
A process is provided for welding a gamma-prime precipitation-strengthened nickel base superalloy by heating the weld area and adjacent region to a ductile temperature, welding while maintaining the entire weld area and adjacent region at the ductile temperature and holding the weldment, weld area and adjacent region at the ductile temperature until the entire weld has solidified. The ductile temperature is above the aging temperature but below the incipient melting temperature of the superalloy.
Thomas H Milidantri from Goshen, NY Get Report