Thomas H Milidantri

20060085978, Apr 27, 2006

Oct 21, 2004

10/970560

Thomas Milidantri - Goshen NY, US

B23P 6/00

029889100, 029402010, 029402190, 029889200, 029889230

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.

20140003948, Jan 2, 2014

Jun 14, 2013

13/917876

Gregory Alan Dubs - Palm Beach Gardens FL, US
Thomas Horace Milidantri - Jensen Beach FL, US

F01D 5/00

416189, 298891

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.

51060108, Apr 21, 1992

Sep 28, 1990

7/590220

Richard J. Stueber - Suffern NY
Thomas Milidantri - Monsey NY
Moshen Tadayon - Washingtonville NY

Chromalloy Gas Turbine Corporation - Orangeburg NY

B23K 3102

228232

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.

53743199, Dec 20, 1994

Nov 4, 1991

7/787546

Richard J. Stueber - Suffern NY
Thomas Milidantri - Monsey NY
Moshen Tadayon - Washingtonville NY

Chromalloy Gas Turbine Corporation - Orangeburg NY

C22C 2706

148404

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.