Jonathan J Stow from 4777 Cincinnati Brookville Rd, Hamilton, OH 45013, age 78, Phone: (513)2565645

Name / Title

Company / Classification

Phones & Addresses

Jonathan Stow
Co-Owner

Plas Cadnant
Hotel/Motel Operation

4777 Cncnnati Brkville Rd, Hamilton, OH 45013
4777 Cincinnati Brookville Rd, Hamilton, OH 45013
(513)7384180

Resumes

Pensioner

view source

Location:

Hamilton, OH

Industry:

Airlines/Aviation

Work:

Ge Aviation
Pensioner
Rolls-Royce Jul 1967 - Jul 1979
Project Development Engineer Rb211

Education:

Ucl 1963 - 1967
Bachelors, Mechanical Engineering Wimbledon College United Kingdom 1957 - 1963

Skills:

Aviation
Lean Manufacturing
Aerospace
Engineering Management
Six Sigma
Process Improvement
Engineering
Continuous Improvement
Aircraft
Systems Engineering
Root Cause Analysis
Manufacturing
Troubleshooting Poor Perfromance In Overhauled Jet Engines

Us Patents

Turbine Airfoil With Separately Formed Tip And Method For Manufacture And Repair Thereof
view source
US Patent:

6558119, May 6, 2003
Filed:

May 29, 2001
Appl. No.:

09/867213
Inventors:

Jonathan James Stow - Hamilton OH
John Peter Heyward - Loveland OH
John Howard Starkweather - Cincinnati OH
Lawrence Joseph Roedl - West Chester OH
Assignee:

General Electric Company - Schenectady NY
International Classification:

F04D 2958
US Classification:

416 97R
Abstract:

An airfoil for a gas turbine engine, the airfoil having a core body with an airfoil body, an integral partial height squealer tip, and an integral tip cap between the airfoil body and the integral partial height squealer tip; and a squealer tip extension bonded to the partial height squealer tip. A method for manufacture and repair of an airfoil.

Turbine Airfoil And Method For Manufacture And Repair Thereof
view source
US Patent:

6595749, Jul 22, 2003
Filed:

Aug 28, 2001
Appl. No.:

09/940812
Inventors:

Lawrence Joseph Roedl - West Chester OH
Jonathan James Stow - Hamilton OH
Assignee:

General Electric Company - Schenectady NY
International Classification:

F01D 518
US Classification:

416 97R, 416224, 416241, 4151731
Abstract:

An airfoil for a gas turbine engine, the airfoil having a core body with an airfoil body, an integral partial height squealer tip defining a tip shelf, and an integral tip cap between the airfoil body and the integral partial height squealer tip; and a squealer tip extension bonded to the partial height squealer tip. A method for manufacture and repair of an airfoil.

Shroud Assembly And Method Of Machining Same
view source
US Patent:

6409471, Jun 25, 2002
Filed:

Feb 16, 2001
Appl. No.:

09/785765
Inventors:

Jonathan J. Stow - Hamilton OH
Assignee:

General Electric Company - Schenectady NY
International Classification:

F01D 1108
US Classification:

4151731, 298882, 2988822
Abstract:

A method of machining an inner surface of a shroud assembly extending generally circumferentially around a central axis of a gas turbine aircraft engine. The method includes determining pre-machined radial clearances during flight between tips of rotor blades in the engine and the inner surface of the shroud assembly at each of a plurality of circumferentially spaced locations around the shroud assembly. The inner surface of the shroud assembly is machined based on the pre-machined radial clearances to provide a generally uniform post-machined radial clearance during flight between the tips of the rotor blades and the inner surface of the shroud assembly at each of the circumferentially spaced locations around the shroud assembly.